Patent Grant
10727611
The present disclosure relates to a waveguide device and an antenna array.
An antenna device including one or more antenna elements (hereinafter also referred to “radiating elements”) that are arrayed on a line or a plane finds its use in various applications, e.g., radar and communication systems. In order to radiate electromagnetic waves from an antenna device, it is necessary to supply electromagnetic waves (e.g., radio-frequency signal waves) to an antenna element, from a circuit which generates electromagnetic waves. Supply of an electromagnetic wave is performed via a waveguide. A waveguide is also used to send electromagnetic waves that are received at the antenna elements to a reception circuit.
Conventionally, feed to an antenna element has often been achieved by using a microstrip line(s). However, in the case where the frequency of an electromagnetic wave to be transmitted or received is a high frequency, e.g., above gigahertz (GHz), a microstrip line will incur a large dielectric loss, thus detracting from the efficiency of the antenna. Therefore, in such a radio frequency region, an alternative waveguide to replace a microstrip line is needed.
Using a hollow waveguide, instead of a microstrip line, to feed each antenna element allows the loss to be reduced even in frequency regions exceeding 30 GHz. A hollow waveguide is a metal body having a circular or rectangular cross section. In the interior of a hollow waveguide, an electromagnetic field mode which is adapted to the shape and size of the body is created. For this reason, an electromagnetic wave is able to propagate within the body in a certain electromagnetic field mode. Since the body interior is hollow, no dielectric loss problem occurs even if the frequency of the electromagnetic wave to propagate increases. However, by using a hollow waveguide, it is difficult to dispose antenna elements with a high density, because the hollow portion of a hollow waveguide needs to have a width which is equal to or greater than a half wavelength of the electromagnetic wave to be propagated, and the body (metal wall) of the hollow waveguide itself also needs to be thick enough. An antenna device utilizing a hollow waveguide is disclosed in Patent Document 1, for example.
On the other hand, examples of waveguiding structures including an artificial magnetic conductor are disclosed in Patent Documents 2 to 4 and Non-Patent Documents 1 and 2. An artificial magnetic conductor is a structure which artificially realizes the properties of a perfect magnetic conductor (PMC), which does not exist in nature. One property of a perfect magnetic conductor is that “a magnetic field on its surface has zero tangential component”. This property is the opposite of the property of a perfect electric conductor (PEC), i.e., “an electric field on its surface has zero tangential component”. Although no perfect magnetic conductor exists in nature, it can be embodied by an artificial structure, e.g., an array of a plurality of electrically conductive rods. An artificial magnetic conductor functions as a perfect magnetic conductor in a specific frequency band which is defined by its structure. An artificial magnetic conductor restrains or prevents an electromagnetic wave of any frequency that is contained in the specific frequency band (propagation-restricted band) from propagating along the surface of the artificial magnetic conductor. For this reason, the surface of an artificial magnetic conductor may be referred to as a high impedance surface.
In the waveguide devices disclosed in Patent Documents 2 to 4 and Non-Patent Documents 1 and 2, an artificial magnetic conductor is realized by a plurality of electrically conductive rods which are arrayed along row and column directions. Such rods may also be referred to as posts or pins. Each of these waveguide devices includes, as a whole, a pair of opposing electrically conductive plates. One conductive plate has a ridge protruding toward the other conductive plate, and stretches of an artificial magnetic conductor extending on both sides of the ridge. An upper face (i.e., its electrically conductive face) of the ridge opposes, via a gap, a conductive surface of the other conductive plate. An electromagnetic wave of a wavelength which is contained in the propagation-restricted band of the artificial magnetic conductor propagates along the ridge, in the space (gap) between this conductive surface and the upper face of the ridge.
In any waveguide device or antenna device, there is a desire to improve its performance, and permit freer positioning of constituent elements.
An antenna array according to an implementation of the present disclosure comprises an electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side. The electrically conductive member has a plurality of slots forming a row along a first direction. The first electrically conductive surface of the electrically conductive member is shaped so as to define a plurality of horns each communicating with a corresponding one of the plurality of slots. E planes of the plurality of slots are on a same plane, or on a plurality of planes which are substantially parallel to one another. The plurality of slots include a first slot and a second slot which are adjacent to each other. The plurality of horns include a first horn communicating with the first slot and a second horn communicating with the second slot. In an E-plane cross section of the first horn, a length from one of two intersections between the E plane and an edge of the first slot to one of two intersections between the E plane and an edge of the aperture plane of the first horn is longer than a length from the other intersection between the E plane and the edge of the first slot to the other intersection between the E plane and the edge of the aperture plane of the first horn, the lengths extending along an inner wall surface of the first horn. In an E-plane cross section of the second horn, a length from one of two intersections between the E plane and an edge of the second slot to one of two intersections between the E plane and an edge of the aperture plane of the second horn is equal to or less than a length from the other intersection between the E plane and the edge of the second slot to the other intersection between the E plane and the edge of the aperture plane of the second horn, the lengths extending along an inner wall surface of the second horn. An axis which passes through a center of the first slot and through a center of the aperture plane of the first horn and an axis which passes through a center of the second slot and through a center of the aperture plane of the second horn are oriented in different directions.
An antenna array according to another implementation of the present disclosure comprises an electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side. The electrically conductive member has a plurality of slots forming a row along a first direction. The first electrically conductive surface of the electrically conductive member is shaped so as to define a plurality of horns each communicating with a corresponding one of the plurality of slots. E planes of the plurality of slots are on a same plane, or on a plurality of planes which are substantially parallel to one another. The plurality of horns include a first horn, a second horn, and a third horn forming a row along the first direction. When electromagnetic waves are supplied to first to third slots respectively communicating with the first to third horns, three main lobes respectively radiated from the first to third horns overlap one another, center axes of the three main lobes are oriented in respectively different directions, and differences among the directions of the center axes of the three main lobes are smaller than a width of each of the three main lobes.
A waveguide device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side; a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; and a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. The second electrically conductive member includes a port at a position adjacent to one end of the waveguide member, the port communicating from the fourth electrically conductive surface to the waveguide, and a choke structure at a position opposing the one end of the waveguide member via the port. The choke structure includes an electrically-conductive ridge at a position adjacent to the port and includes one or more electrically conductive rods provided on the third electrically conductive surface with a gap from a farther end of the ridge from the port. When an electromagnetic wave propagating in the waveguide has a central wavelength λ0 in free space, the ridge has a length equal to or greater than λ0/16 and less than λ0/4 in a direction along the waveguide.
A waveguide device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side; a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. The first electrically conductive member includes a port provided at a position opposing a portion of the waveguide face adjacent to one end of the waveguide member, the port communicating from the first electrically conductive surface to the second electrically conductive surface. The second electrically conductive member includes a choke structure in a region containing the one end of the waveguide member. The choke structure comprises a waveguide member end portion and one or more electrically conductive rods, the waveguide member end portion spanning from an edge of an opening of the port to an edge of the one end of the waveguide member as projected onto the waveguide face, the one or more electrically conductive rods being provided on the third electrically conductive surface with a gap from the one end of the waveguide member. When an electromagnetic wave propagating in the waveguide has a central wavelength λ0 in free space, the waveguide member end portion has a length equal to or greater than λ0/16 and less than λ0/4 in a direction along the waveguide.
A waveguide device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side; a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. The second electrically conductive member includes a port at a position adjacent to one end of the waveguide member, the port communicating from the fourth electrically conductive surface to the waveguide, and a choke structure at a position opposing the one end of the waveguide member via the port. The choke structure includes an electrically-conductive ridge at a position adjacent to the port and includes one or more electrically conductive rods provided on the third electrically conductive surface with a gap from a farther end of the ridge from the port. The ridge includes a first portion adjacent to the port and a second portion adjacent to the first portion. A distance between the first portion and the second electrically conductive surface is longer than a distance between the second portion and the second electrically conductive surface.
A waveguide device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side; a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. The first electrically conductive member includes a port provided at a position opposing a portion of the waveguide face adjacent to one end of the waveguide member, the port communicating from the first electrically conductive surface to the second electrically conductive surface. The second electrically conductive member includes a choke structure in a region containing the one end of the waveguide member. The choke structure comprises a waveguide member end portion and one or more electrically conductive rods, the waveguide member end portion spanning from an edge of an opening of the port to an edge of the one end of the waveguide member as projected onto the waveguide face, the one or more electrically conductive rods being provided on the third electrically conductive surface with a gap from the one end of the waveguide member. At a site opposing the waveguide member end portion, the second electrically conductive surface of the first electrically conductive member includes a first portion adjacent to the port and a second portion adjacent to the first portion. A distance between the first portion and the waveguide face is longer than a distance between the second portion and the waveguide face.
A waveguide device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side; a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. The second electrically conductive member includes a port communicating from the fourth electrically conductive surface to the waveguide. The waveguide member is spatially separated into a first portion and a second portion at the port. A portion of an inner wall of the port connects to one end of the first portion of the waveguide member. Another portion of the inner wall of the port connects to one end the second portion of the waveguide member. An intra-waveguide member gap defined between two opposing end faces at the one end of the first portion and the one end of the second portion of the waveguide member includes a narrow portion which is smaller in size than a gap between the portion of the inner wall of the port that connects to the first portion of the waveguide member and the other portion of the inner wall of the port that connects to the second portion of the waveguide member.
An array antenna device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, the first electrically conductive member having a plurality of slots; a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. The second electrically conductive member includes a port communicating from the fourth electrically conductive surface to the waveguide. On the second electrically conductive surface, a first slot and a second slot which are adjacent to each other among the plurality of slots are at symmetric positions with respect to a center of the port. The waveguide member includes a pair of impedance matching structures adjoining the port, each of the pair of impedance matching structures having a flat portion adjoining the port and a dent adjoining the flat portion, and partly opposes one of the first and second slots.
An array antenna device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side; a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. The second electrically conductive member includes a port communicating from the fourth electrically conductive surface to the waveguide. The waveguide member is spatially separated into a first portion and a second portion at the port. A portion of an inner wall of the port connects to one end of the first portion of the waveguide member. Another portion of the inner wall of the port connects to one end the second portion of the waveguide member. A distance between two opposing end faces at the one end of the first portion and the one end of the second portion of the waveguide member is different from a distance between the portion of the inner wall of the port that connects to the first portion of the waveguide member and the other portion of the inner wall of the port that connects to the second portion of the waveguide member.
An array antenna device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, the first electrically conductive member having a plurality of slots; a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. The second electrically conductive member includes a port communicating from the fourth electrically conductive surface to the waveguide. The plurality of slots opposes the waveguide face. On the second electrically conductive surface, a first slot and a second slot which are adjacent to each other among the plurality of slots are at symmetric positions with respect to a center of the port. The first electrically conductive surface of the first electrically conductive member is shaped so as to define a plurality of horns respectively communicating with the plurality of slots. Among the plurality of horns, a distance between centers of the openings of two adjacent horns is shorter than a distance on the second electrically conductive surface from a center of the first slot to a center of the second slot.
An array antenna device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side; a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. The second electrically conductive member includes a port at a position adjacent to one end of the waveguide member, the port communicating from the fourth electrically conductive surface to the waveguide, and a choke structure at a position opposing the one end of the waveguide member via the port. The choke structure includes a first portion adjacent to the port and a second portion adjacent to the first portion. A distance between the first portion and the second electrically conductive surface is longer than a distance between the second portion and the second electrically conductive surface.
An array antenna device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, the first electrically conductive member having 2N (where N is an integer of 2 or greater) ports; a waveguide member at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face opposing the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, and the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide in a gap between the second electrically conductive surface and the waveguide face. Via combinations among a plurality of T-branching portions, the waveguide member branches from one stem into 2N waveguide terminal sections, the 2N ports respectively opposing the 2N waveguide terminal sections, at least one of the 2N waveguide terminal sections has a shape which is different from the shape of another.
An array antenna device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side; a waveguide member at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face opposing the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, and the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. Via combinations among a plurality of T-branching portions, the waveguide member branches from one stem into 2N (where N is an integer of 2 or greater) waveguide terminal sections. On a stem portion adjacent to each of the plurality of T-branching portions, the waveguide member includes a plurality of impedance transforming sections to increase a capacitance of the waveguide. Among the plurality of impedance transforming sections, a length of a first impedance transforming section in a direction along the waveguide is shorter than a length of a second impedance transforming section in a direction along the waveguide, the first impedance transforming section being relatively far from the waveguide terminal section, the second impedance transforming section being relatively close to the waveguide terminal section.
An array antenna device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side; a waveguide member at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face opposing the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor having a plurality of electrically conductive rods on the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. The second electrically conductive member includes a rectangular hollow-waveguide at a position adjacent to one end of the waveguide member, the rectangular hollow-waveguide communicating from the fourth electrically conductive surface to the waveguide, and a choke structure at a position opposing the one end of the waveguide member via the rectangular hollow-waveguide. The plurality of electrically conductive rods include at least two rows of electrically conductive rods that are arrayed on both sides of the waveguide member and extending along the waveguide member. As viewed from a normal direction of the third electrically conductive surface, the rectangular hollow-waveguide has a rectangular shape which is defined by a pair of longer sides and a pair of shorter sides orthogonal to the longer sides, one of the pair of longer sides being in contact with the one end of the waveguide member, and a length of each longer side of the rectangular hollow-waveguide is longer than twice a shortest distance between centers of the at least two rows of electrically conductive rods, and shorter than 3.5 times the shortest distance between the centers.
An array antenna device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, the first electrically conductive member having a plurality of slots; a waveguide member at the rear side of the first electrically conductive member, having an electrically-conductive waveguide face in a stripe shape opposing the second electrically conductive surface and at least one of the plurality of slots, the waveguide member extending in a manner of following along the second electrically conductive surface; and a second electrically conductive member at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, and the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface; and an artificial magnetic conductor extending on both sides of the waveguide member and being provided on the third electrically conductive surface, the artificial magnetic conductor having a plurality of electrically conductive rods on the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. At least one of a distance from the second electrically conductive surface to the waveguide face and a width of the waveguide face varies along the waveguide. Among the plurality of electrically conductive rods, a plurality of first electrically conductive rods adjacent to the waveguide member are in a periodic array with a first period in a direction along the waveguide. Among the plurality of electrically conductive rods, a plurality of second electrically conductive rods not adjacent to the waveguide member are in a periodic array with a second period in a direction along the waveguide, the second period being longer than the first period.
An array antenna device according to another implementation of the present disclosure comprises: a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, the first electrically conductive member having a plurality of slots; a waveguide member at the rear side of the first electrically conductive member, having an electrically-conductive waveguide face in a stripe shape opposing the second electrically conductive surface and at least one of the plurality of slots, the waveguide member extending in a manner of following along the second electrically conductive surface; a second electrically conductive member at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, and the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface; and an artificial magnetic conductor extending on both sides of the waveguide member and being provided on the third electrically conductive surface, the artificial magnetic conductor having a plurality of electrically conductive rods on the third electrically conductive surface. The second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face. In a plane which is parallel to the second electrically conductive member, a first direction is defined as a direction extending along the waveguide, and a second direction is defined perpendicular to the first direction. Among the plurality of electrically conductive rods, a group of rods adjacent to the waveguide member each have a dimension along the first direction which is larger than a dimension along the second direction.
These general and specific aspects may be implemented using a system, a method, and a computer program, and any combination of systems, methods, and computer programs.
Additional benefits and advantages of the disclosed embodiments will be apparent from the specification and Figures. The benefits and/or advantages may be individually provided by the various embodiments and features of the specification and drawings disclosure, and need not all be provided in order to obtain one or more of the same.
According to an embodiment of the present disclosure, it is possible to enhance the performance of a waveguide device or antenna device, and permit freer positioning of constituent elements thereof.
Prior to describing embodiments of the present disclosure, findings that form the basis of the present disclosure will be described.
Embodiments of the present disclosure provide improvements on waveguide devices or antenna devices in which a conventional hollow waveguide(s) or a ridge waveguide(s) is utilized. First, a fundamental construction of a waveguide device in which a ridge waveguide(s) is utilized will be described.
A ridge waveguide which is disclosed in each of the aforementioned Patent Document 2 and Non-Patent Document 1, etc., is provided in a waffle iron structure which may function as an artificial magnetic conductor. A ridge waveguide in which such an artificial magnetic conductor is utilized (which hereinafter may be referred to as a WRG: Waffle-iron Ridge waveguide) according to the present disclosure is able to realize an antenna feeding network with low losses in the microwave or the millimeter wave band.
Note that any structure appearing in a figure of the present application is shown in an orientation that is selected for ease of explanation, which in no way should limit its orientation when an embodiment of the present disclosure is actually practiced. Moreover, the shape and size of a whole or a part of any structure that is shown in a figure should not limit its actual shape and size.
See
On the conductive member 120, a ridge-like waveguide member 122 is provided among the plurality of conductive rods 124. More specifically, stretches of an artificial magnetic conductor are present on both sides of the waveguide member 122, such that the waveguide member 122 is sandwiched between the stretches of artificial magnetic conductor on both sides. As can be seen from
On both sides of the waveguide member 122, the space between the surface 125 of each stretch of artificial magnetic conductor and the conductive surface 110a of the conductive member 110 does not allow an electromagnetic wave of any frequency that is within a specific frequency band to propagate. This frequency band is called a “prohibited band”. The artificial magnetic conductor is designed so that the frequency of an electromagnetic wave (which hereinafter may be referred to as a signal wave) to propagate in the waveguide device 100 (which may hereinafter be referred to as the “operating frequency”) is contained in the prohibited band. The prohibited band may be adjusted based on the following: the height of the conductive rods 124, i.e., the depth of each groove formed between adjacent conductive rods 124; the width of each conductive rod 124; the interval between conductive rods 124; and the size of the gap between the leading end 124a and the conductive surface 110a of each conductive rod 124.
Next, with reference to
(1) Width of the Conductive Rod
The width (i.e., the size along the X direction and the Y direction) of the conductive rod 124 may be set to less than λm/2. Within this range, resonance of the lowest order can be prevented from occurring along the X direction and the Y direction. Since resonance may possibly occur not only in the X and Y directions but also in any diagonal direction in an X-Y cross section, the diagonal length of an X-Y cross section of the conductive rod 124 is also preferably less than λm/2. The lower limit values for the rod width and diagonal length will conform to the minimum lengths that are producible under the given manufacturing method, but is not particularly limited.
(2) Distance from the Root of the Conductive Rod to the Conductive Surface of the Conductive Member
The distance from the root 124b of each conductive rod 124 to the conductive surface 110a of the conductive member 110 may be longer than the height of the conductive rods 124, while also being less than λm/2. When the distance is λm/2 or more, resonance may occur between the root 124b of each conductive rod 124 and the conductive surface 110a, thus reducing the effect of signal wave containment.
The distance from the root 124b of each conductive rod 124 to the conductive surface 110a of the conductive member 110 corresponds to the spacing between the conductive member 110 and the conductive member 120. For example, when a signal wave of 76.5±0.5 GHz (which belongs to the millimeter band or the extremely high frequency band) propagates in the waveguide, the wavelength of the signal wave is in the range from 3.8923 mm to 3.9435 mm. Therefore, λm equals 3.8923 mm in this case, so that the spacing between the conductive member 110 and the conductive member 120 may be set to less than a half of 3.8923 mm. So long as the conductive member 110 and the conductive member 120 realize such a narrow spacing while being disposed opposite from each other, the conductive member 110 and the conductive member 120 do not need to be strictly parallel. Moreover, when the spacing between the conductive member 110 and the conductive member 120 is less than λm/2, a whole or a part of the conductive member 110 and/or the conductive member 120 may be shaped as a curved surface. On the other hand, the conductive members 110 and 120 each have a planar shape (i.e., the shape of their region as perpendicularly projected onto the XY plane) and a planar size (i.e., the size of their region as perpendicularly projected onto the XY plane) which may be arbitrarily designed depending on the purpose.
Although the conductive surface 120a is illustrated as a plane in the example shown in
(3) Distance L2 from the Leading End of the Conductive Rod to the Conductive Surface
The distance L2 from the leading end 124a of each conductive rod 124 to the conductive surface 110a is set to less than λm/2. When the distance is λm/2 or more, a propagation mode in which an electromagnetic wave reciprocates between the leading end 124a of each conductive rod 124 and the conductive surface 110a may occur, thus no longer being able to contain an electromagnetic wave. Note that, among the plurality of conductive rods 124, at least those which are adjacent to the waveguide member 122 do not have their leading ends in electrical contact with the conductive surface 110a. As used herein, the leading end of a conductive rod not being in electrical contact with the conductive surface means either of the following states: there being an air gap between the leading end and the conductive surface; or the leading end of the conductive rod and the conductive surface adjoining each other via an insulating layer which may exist in at least one of the leading end of the conductive rod or in the conductive surface.
(4) Arrangement and Shape of Conductive Rods
The interspace between two adjacent conductive rods 124 among the plurality of conductive rods 124 has a width of less than λm/2, for example. The width of the interspace between any two adjacent conductive rods 124 is defined by the shortest distance from the surface (side face) of one of the two conductive rods 124 to the surface (side face) of the other. This width of the interspace between rods is to be determined so that resonance of the lowest order will not occur in the regions between rods. The conditions under which resonance will occur are determined based by a combination of: the height of the conductive rods 124; the distance between any two adjacent conductive rods; and the capacitance of the air gap between the leading end 124a of each conductive rod 124 and the conductive surface 110a. Therefore, the width of the interspace between rods may be appropriately determined depending on other design parameters. Although there is no clear lower limit to the width of the interspace between rods, for manufacturing ease, it may be e.g. λm/16 or more when an electromagnetic wave in the extremely high frequency range is to be propagated. Note that the interspace does not need to have a constant width. So long as it remains less than λm/2, the interspace between conductive rods 124 may vary.
The arrangement of the plurality of conductive rods 124 is not limited to the illustrated example, so long as it exhibits a function of an artificial magnetic conductor. The plurality of conductive rods 124 do not need to be arranged in orthogonal rows and columns; the rows and columns may be intersecting at angles other than 90 degrees. The plurality of conductive rods 124 do not need to form a linear array along rows or columns, but may be in a dispersed arrangement which does not present any straightforward regularity. The conductive rods 124 may also vary in shape and size depending on the position on the conductive member 120.
The surface 125 of the artificial magnetic conductor that are constituted by the leading ends 124a of the plurality of conductive rods 124 does not need to be a strict plane, but may be a plane with minute rises and falls, or even a curved surface. In other words, the conductive rods 124 do not need to be of uniform height, but rather the conductive rods 124 may be diverse so long as the array of conductive rods 124 is able to function as an artificial magnetic conductor.
Each conductive rod 124 does not need to have a prismatic shape as shown in the figure, but may have a cylindrical shape, for example. Furthermore, each conductive rod 124 does not need to have a simple columnar shape. The artificial magnetic conductor may also be realized by any structure other than an array of conductive rods 124, and various artificial magnetic conductors are applicable to the waveguide device of the present disclosure. Note that, when the leading end 124a of each conductive rod 124 has a prismatic shape, its diagonal length is preferably less than λm/2. When the leading end 124a of each conductive rod 124 is shaped as an ellipse, the length of its major axis is preferably less than λm/2. Even when the leading end 124a has any other shape, the dimension across it is preferably less than λm/2 even at the longest position.
The height of each conductive rod 124, i.e., the length from the root 124b to the leading end 124a, may be set to a value which is shorter than the distance (i.e., less than λm/2) between the conductive surface 110a and the conductive surface 120a, e.g., λ0/4.
(5) Width of the Waveguide Face
The width of the waveguide face 122a of the waveguide member 122, i.e., the size of the waveguide face 122a along a direction which is orthogonal to the direction that the waveguide member 122 extends, may be set to less than λm/2 (e.g. λ0/8). If the width of the waveguide face 122a is λm/2 or more, resonance will occur along the width direction, which will prevent any WRG from operating as a simple transmission line.
(6) Height of the Waveguide Member
The height (i.e., the size along the Z direction in the example shown in the figure) of the waveguide member 122 is set to less than λm/2. The reason is that, if the distance is λm/2 or more, the distance between the root 124b of each conductive rod 124 and the conductive surface 110a will be λm/2 or more. Similarly, the height of the conductive rods 124 (especially those conductive rods 124 which are adjacent to the waveguide member 122) is set to less than λm/2.
(7) Distance L1 Between the Waveguide Face and the Conductive Surface
The distance L1 between the waveguide face 122a of the waveguide member 122 and the conductive surface 110a is set to less than λm/2. If the distance is λm/2 or more, resonance will occur between the waveguide face 122a and the conductive surface 110a, which will prevent functionality as a waveguide. In one example, the distance is λm/4 or less. In order to ensure manufacturing ease, when an electromagnetic wave in the extremely high frequency range is to propagate, the distance L1 is preferably λm/16 or more, for example.
The lower limit of the distance L1 between the conductive surface 110a and the waveguide face 122a and the lower limit of the distance L2 between the conductive surface 110a and the leading end 124a of each conductive rod 124 depends on the machining precision, and also on the precision when assembling the two upper/lower conductive members 110 and 120 so as to be apart by a constant distance. When a pressing technique or an injection technique is used, the practical lower limit of the aforementioned distance is about 50 micrometers (μm). In the case of using an MEMS (Micro-Electro-Mechanical System) technique to make a product in e.g. the terahertz range, the lower limit of the aforementioned distance is about 2 to about 3 μm.
In the waveguide device 100 of the above-described construction, a signal wave of the operating frequency is unable to propagate in the space between the surface 125 of the artificial magnetic conductor and the conductive surface 110a of the conductive member 110, but propagates in the space between the waveguide face 122a of the waveguide member 122 and the conductive surface 110a of the conductive member 110. Unlike in a hollow waveguide, the width of the waveguide member 122 in such a waveguide structure does not need to be equal to or greater than a half of the wavelength of the electromagnetic wave to propagate. Moreover, the conductive member 110 and the conductive member 120 do not need to be interconnected by a metal wall that extends along the thickness direction (i.e., in parallel to the YZ plane).
On both sides of the waveguide member 122, stretches of artificial magnetic conductor that are created by the plurality of conductive rods 124 are present. An electromagnetic wave propagates in the gap between the waveguide face 122a of the waveguide member 122 and the conductive surface 110a of the conductive member 110.
In the waveguide structure of
For reference,
For reference's sake,
On the other hand, a waveguide device 100 including an artificial magnetic conductor can easily realize a structure in which waveguide members 122 are placed close to one another. Thus, such a waveguide device 100 can be suitably used in an array antenna device that includes plural antenna elements in a close arrangement.
Although the present disclosure mainly describes examples of utilizing a ridge waveguide which includes an artificial magnetic conductor, conventional hollow waveguides can be utilized in some embodiments. Such embodiments will be described later as variants of Embodiment 2.
Next, an exemplary construction of a slot array antenna device utilizing the aforementioned waveguide structure will be described. A “slot array antenna device” is defined as an array antenna device which includes a plurality of slots as antenna elements. In the following description, a slot array antenna device may simply be referred to as an array antenna device.
To the waveguide extending between each waveguide member 122 and the conductive surface 110a, an electromagnetic wave is supplied from a transmission circuit not shown. In this example, the interval between the centers of slots 112 along the Y direction is designed to be the same value as the wavelength of an electromagnetic wave propagating in the waveguide. As a result, electromagnetic waves with an phase are radiated from the six slots 112 placed side-by-side along the Y direction.
As has been described with reference to
In the construction of
Hereinafter, the construction of the slot array antenna device 300 will be described in more detail.
The slot array antenna device 300 includes a plate-like first conductive member 110 and a plate-like second conductive member 120, which are in opposing and parallel positions to each other. The first conductive member 110 includes a plurality of slots 112 which are arrayed along a first direction (the Y direction) and a second direction (the X direction) that intersects (or, in this example, is orthogonal to) the first direction. A plurality of conductive rods 124 are arrayed on the second conductive member 120.
The conductive surface 110a of the first conductive member 110 has a two-dimensional expanse along a plane which is orthogonal to the axial direction (Z direction) of the conductive rods 124 (i.e., a plane which is parallel to the XY plane). Although the conductive surface 110a is shown to be a smooth plane in this example, the conductive surface 110a does not need to be a smooth plane, but may be curved or include minute rises and falls, as will be described later. The plurality of conductive rods 124 and the plurality of waveguide members 122 are connected to the second conductive surface 120a.
The waveguide face 122a of each waveguide member 122 shown in
Each conductive rod 124 does not need to be entirely electrically conductive, so long as it at least includes an electrically conductive layer that extends along the upper face and the side face of the rod-like structure. Although this electrically conductive layer may be located at the surface layer of the rod-like structure, the surface layer may be composed of an insulation coating or a resin layer with no electrically conductive layer existing on the surface of the rod-like structure. Moreover, each second conductive member 120 does not need to be entirely electrically conductive, so long as it can support the plurality of conductive rods 124 to constitute an artificial magnetic conductor. Of the surfaces of the second conductive member 120, a face 120a carrying the plurality of conductive rods 124 may be electrically conductive, such that the surfaces of adjacent ones of the plurality of conductive rods 124 are electrically connected. Moreover, the electrically conductive layer of the second conductive member 120 may be covered with insulation coating or a resin layer. In other words, the entire combination of the second conductive member 120 and the plurality of conductive rods 124 may at least present an electrically conductive layer with rises and falls opposing the conductive surface 110a of the first conductive member 110.
In this example, the entire first conductive member 110 is composed of an electrically conductive material, and each slot 112 is an opening made in the first conductive member 110. However, slot the 112 is not limited to such a structure. For example, in a construction where the first conductive member 110 includes an internal dielectric layer and a superficial electrically conductive layer, the opening may only extend through the electrically conductive layer, and not through the dielectric layer, and this structure will still function as a slot.
The waveguide extending between the first conductive member 110 and each waveguide member 122 is open at both ends. Although not shown in
The preferable length of an additional transmission line in a choke structure has been believed to be λr/4, where λr is the wavelength of a signal wave on the transmission line. However, the inventors have found that electromagnetic wave leakage can be suppressed and good functionality can be attained even when the length of an additional transmission line in a choke structure is shorter than λr/4. In actuality, it is more preferable that the length of the additional transmission line is equal to or less than λ0/4, which is even shorter than λr/4. In an embodiment according to the present disclosure, the length of the additional transmission line may be se to equal to or greater than λ0/16 and less than λ0/4. Examples of such construction will be later described as Embodiment 3.
Although not shown, the waveguiding structure in the slot array antenna device 300 has a port (opening) that is connected to a transmission circuit or reception circuit (i.e., an electronic circuit) not shown. The port may be provided at one end or an intermediate position (e.g., a central portion) of each waveguide member 122 shown in
In this example, two adjacent slots 112 along the X direction are excited with an equiphase. Therefore, the feeding path is arranged so that the transmission distances from the transmission circuit to two such slots 112 are equal. More preferably, two such slots 112 are excited with an equiphase and equiamplitude. Furthermore, the distance between the centers of two adjacent slots 112 along the Y direction is designed equal to the wavelength λg in the waveguide. As a result of this, electromagnetic waves with an equiphase are radiated from all slots 112, whereby a transmission antenna with a high gain can be realized.
Note that the interval between the centers of two adjacent slots along the Y direction may have a different value from that of the wavelength λg. This will allow a phase difference to occur at the positions of the plurality of slots 112, so that the azimuth at which the radiated electromagnetic waves will strengthen one another can be shifted from the frontal direction to another azimuth in the YZ plane. Thus, with the slot antenna 200 shown in
An array antenna device including a two-dimensional array of such plural slots 112 on a plate-like conductive member 110 may also be called a flat panel array antenna device. Depending on the purpose, the plurality of slot rows placed side-by-side along the X direction may vary in length (i.e., in terms of distance between the slots at both ends of each slot row). A staggered array may be adopted such that, between two adjacent rows along the X direction, the positions of the slots are shifted along the Y direction. Depending on the purpose, the plurality of slot rows and the plurality of waveguide members may include portions which are not parallel but are angled. Without being limited to an implementation where the waveguide face 122a of each waveguide member 122 opposes all of the slots 112 being placed side-by-side along the Y direction, it suffices if each waveguide face 122a opposes at least one slot among the plural slots that are placed side-by-side along the Y direction.
In the examples shown in
In the array antenna device shown 300a in the figures, a first waveguide device 100a and a second waveguide device 100b are layered. The first waveguide device 100a includes waveguide members 122U that directly couple to slots 112. The second waveguide device 100b includes a further waveguide member 122L that couples to the waveguide members 122U of the first waveguide device 100a. The waveguide member 122L and the conductive rods 124L of the second waveguide device 100b are arranged on a third conductive member 140. The second waveguide device 100b is basically similar in construction to the first waveguide device 100a.
As shown in
The waveguide members 122U of the first waveguide device 100a couple to the waveguide member 122L of the second waveguide device 100b, through ports (openings) 145U that are provided in the second conductive member 120. Stated otherwise, an electromagnetic wave which has propagated through the waveguide member 122L of the second waveguide device 100b passes through a port 145U to reach a waveguide member 122U of the first waveguide device 100a, and propagates through the waveguide member 122U of the first waveguide device 100a. In this case, each slot 112 functions as an antenna element (radiating element) to allow an electromagnetic wave which has propagated through the waveguide to be radiated into space. Conversely, when an electromagnetic wave which has propagated in space impinges on a slot 112, the electromagnetic wave couples to the waveguide member 122U of the first waveguide device 100a that lies directly under that slot 112, and propagates through the waveguide member 122U of the first waveguide device 100a. An electromagnetic wave which has propagated through a waveguide member 122U of the first waveguide device 100a may also pass through a port 145U to reach the waveguide member 122L of the second waveguide device 100b, and propagates through the waveguide member 122L of the second waveguide device 100b. Via a port 145L of the third conductive member 140, the waveguide member 122L of the second waveguide device 100b may couple to an external waveguide device or radio frequency circuit (electronic circuit). As one example,
The first conductive member 110 shown in
In the array antenna of this example, as can be seen from
With the waveguide member 122L shown in
Depending on the purpose, it is not necessary for all slots 112 functioning as antenna elements to radiate electromagnetic waves in the same phase. In the construction shown in
The electronic circuit 310 is connected to a waveguide extending above each waveguide member 122U, via the ports 145U and 145L shown in
Next, variants of the horn 114 will be described. Without being limited to what is illustrated in
The inventors have found the following to be effective in enhancing the performance of the aforementioned array antenna device or waveguide device.
(1) Suppressing unwanted signal wave reflection at each port 145U that couples the waveguide in the excitation layer and the waveguide in the distribution layer.
(2) Ensuring that the distance between the centers of horns is different from the distance between the centers of slots, thus optimizing the directivity of the antenna array and/or providing an improved design freedom; this improvement is applicable not only to a horn antenna array in which the aforementioned WRG structure is used, but also to a horn antenna array in which the hollow waveguide structure is used.
(3) Using a different choke structure from conventionally, to suppress unwanted reflection when propagating an electromagnetic wave via each port.
(4) Adjusting the shape of a waveguide member having a plurality of branching portions to control an in-plane distribution of the excitation amplitude of the array antenna.
(5) Adjusting the shape of a waveguide member having a plurality of branching portions to reduce propagation losses.
(6) Improving the performance of the hollow waveguide that couples any electronic circuitry (e.g., MMIC) and the waveguide device.
(7) Providing a new array pattern for the rods, as adapted to the interval between the waveguide members 122U and 122L.
Hereinafter, more specific exemplary constructions for array antenna devices according to embodiments of the present disclosure will be described. Note however that unnecessarily detailed descriptions may be omitted. For example, detailed descriptions on what is well known in the art or redundant descriptions on what is substantially the same constitution may be omitted. This is to avoid lengthy description, and facilitate the understanding of those skilled in the art. The accompanying drawings and the following description, which are provided by the present inventors so that those skilled in the art can sufficiently understand the present disclosure, are not intended to limit the scope of claims. In the following description, any identical or similar constituent elements will be denoted by identical reference numerals.
<Array Antenna Device>
First, with reference to
As shown in
In the present embodiment, the first conductive member 110 has a first conductive surface 110b on the front side and a second conductive surface 110a on the rear side, and has a plurality of slots 112-1, 112-2, 112-3, 112-4, 112-5 and 112-6. These slots may be collectively referred to as the slots 112. Although
The second conductive member 120 is located on the rear side of the first conductive member 110. The second conductive member 120 has a third conductive surface 120a on the front side, which opposes the second conductive surface 110a of the first conductive member 110, and a fourth conductive surface 120b on the rear side. As such, the second conductive member 120 supports the first waveguide member 122U. The first waveguide member 122U has an electrically-conductive waveguide face 122a of a stripe shape that opposes the second conductive surface 110a, and extends linearly along the second conductive surface 110a. On both sides of the linearly-extending first waveguide member 122U (i.e., the frontward and rearward sides in
The second conductive surface 110a of the first conductive member 110, the waveguide face 122a of the first waveguide member 122U, and the artificial magnetic conductor (not shown in
By allowing at least one of the distance from the second conductive surface 110a to the waveguide face 122a and the width of the waveguide face 122a to vary as appropriate along the direction that the first waveguide member 122U extends, the wavelength of a signal wave that propagates in this waveguide can be reduced. Assume that a signal wave has a central wavelength λr when both of the distance from the second conductive surface 110a to the waveguide face 122a and the width of the waveguide face 122a are constant along the direction that the first waveguide member 122U extends. When a signal wave of the same frequency propagates in a vacuum, the signal wave has a central wavelength λ0 as described above. In this case, the relationship λr>λ0 holds. However, by forming rises and falls on the waveguide face 122a of the first waveguide member 122U to vary the distance from the second conductive surface 110a to the waveguide face 122a as appropriate, or vary the width of the waveguide face 122a as appropriate, for example, the central wavelength of a signal wave propagating in such a waveguide can be made shorter than λr.
The second conductive member 120 has a port 145U that extends from the third conductive surface 120a through to the fourth conductive surface 120b. The port 145U communicates from the fourth conductive surface 120b to the waveguide extending between the second conductive surface 110a and the waveguide face 122a. In the present specification, when a port is said to “communicate from a conductive surface to a waveguide (i.e., that is associated with another conductive surface)” it is meant that, as viewed from the normal direction of the aperture plane of the port, the inner wall of the port and the side face (end face) at an end of the waveguide member that is associated with the waveguide in question are aligned in position (substantially flush).
Among the plurality of slots 112, a first slot 112-1 and a second slot 112-2, which are adjacent to each other, are at symmetric positions with respect to the center of the port 145U. In the example shown, the entirety of the six slots 112 are positioned symmetrically with respect to the center of the port 145U. The distance between the centers of any two adjacent slots 112 is set equal to the wavelength of a signal wave propagating in the waveguide (or, in the case where the wavelength varies with frequency modulation, its central wavelength). This is in order to supply equiphase signal waves to the respective slots 112. Depending on the intended characteristics of the array antenna, it may need to be designed so that the phase of the signal wave to be supplied to each slot is intentionally made different. In that case, the distance between the centers of two adjacent slots 112 may be chosen to be a length which somewhat differs from the wavelength of a signal wave propagating in the waveguide.
The third conductive member 140 is located on the rear side of the second conductive member 120. The third conductive member 140 has a fifth conductive surface 140a on the front side, which opposes the fourth conductive surface 120b of the second conductive member 120, and a sixth conductive surface 140b on the rear side. As such, the third conductive member 140 supports the second waveguide member 122L. The second waveguide member 122L has an electrically-conductive waveguide face 122a that opposes the fourth conductive surface 120b, and extends along the fourth conductive surface 120b.
On both sides of the second waveguide member 122L, too, is located an artificial magnetic conductor provided on the fifth conductive surface 140a of the third conductive member 140. The fourth conductive surface 120b of the second conductive member 120, the waveguide face 122a of the second waveguide member 120L, and the artificial magnetic conductor (not shown in
In the present embodiment, the first waveguide member 122U has a pair of impedance matching structures 123 adjoining the port 145U. The details of the impedance matching structure 123 will be described later.
In
<Impedance Matching Structures of the Port>
A cross section taken perpendicular to the Z axis of each port 145U may have a variety of shapes. In the present embodiment, as shown in
With reference to
Each of the pair of impedance matching structures 123 according to the present embodiment includes a flat portion 123a adjoining the port 145U and a dent 123b adjoining the flat portion 123a.
The length (La+Lb) of the impedance matching structure 123 along the direction that the waveguide member 122U extends is about λr/2. The length La of the flat portion 123a along the direction that the waveguide member 122U extends is longer than λr/4. The length Lb of the dent 123b along the direction that the waveguide member 122U extends is shorter than the length La of the flat portion 123a. The length Lb is typically set to be shorter than λr/4.
As described earlier, when at least one of the distance from the second conductive surface 110a to the waveguide face 122a and the width of the waveguide face 122a is allowed to vary along the waveguide, the central wavelength of a signal wave propagating in the waveguide can be made shorter than λ0. When the central wavelength of a signal wave propagating in the waveguide is thus shortened, the distance from the center of the first slot 112-1 to the center of the third slot 112-3 can be made shorter than the distance from the center of the first slot 112-1 to the center of the second slot 112-2. Note that the distance from the center of the first slot 112-1 to the center of the third slot 112-3, and the distance from the center of the third slot 112-3 to the center of the fifth slot 112-5, are both set equal to the wavelength (as taken within the waveguide) of a signal wave propagating in the waveguide. Similarly, the distance from the center of the second slot 112-2 to the center of the fourth slot 112-4, and the distance from the center of the fourth slot 112-4 to the center of the sixth slot 112-6, are both set equal to the wavelength (as taken within the waveguide) of a signal wave propagating in the waveguide.
In the present embodiment, the distance between the centers of the first slot 112-1 and the second slot 112-2 is equal to λr. Therefore, it is preferable to adopt the impedance matching structure 123 illustrated in
Next, with reference to
A port 145U shown in the figure is in a position at which the first waveguide member 122U is spatially separated into a first portion 122-1 and a second portion 122-2. Via the port 145U, one end of the first portion 122-1 and one end of the second portion 122-2 oppose each other. A portion of the inner wall of the port 145U is connected to the one end of the first portion 122-1 of the first waveguide member 122U. Another, opposing portion of the inner wall of the port 145U is connected to the one end of the second portion 122-2 of the first waveguide member 122U.
In the example shown in
In this example, a cross section of the port 145U which is orthogonal to the center axis of the port 145U has an H-shape; however, it may have other shapes as will be described later. The center axis of the port 145U is defined as a line which passes through the center of the opening of the port 145U and which is perpendicular to the plane of the opening.
In this example, the narrow portion between the pair of bumps 123c reaches the waveguide face 122a of the waveguide member 122U. Without being limited to the construction shown in
In the example shown in
A structuring include such a bump 123c or dent 123d may be provided in at least either one of the one end of the first portion 122-1 of the first waveguide member 122U and the one end of the second portion 122-2. Alternatively, either one of a bump 123c and a dent 123d may be provided at the one end of the first portion 122-1 of the first waveguide member 122U, while the other may be provided at the one end of the second portion 122-2. Alternatively, a bump 123c and a dent 123d may both be provided at the one end of the first portion 122-1 of the first waveguide member 122U, or a bump 123c and a dent 123d may both be provided at the one end of the second portion 122-2 of the first waveguide member 122U. Although the examples shown in
The impedance matching structure 123 shown in
The various shapes of the port 145U shown in
Hereinafter, with reference to
In
In the present embodiment, by using horns with asymmetric shapes, the distance between the centers of the openings of the two adjacent horns (i.e., the distance between their phase centers) can be made shorter or longer than the distance between the centers of two adjacent slots. For example, in a direction along a waveguide member, the distance between the centers of slots is about λr, but the distance between the centers of horn openings can be made shorter than λ0. This permits freer positioning of constituent elements.
It has conventionally common practice that, in an antenna array including a plurality of horn antennas, all horns be oriented in the same direction, as is disclosed in e.g. Patent Document 1. It has also been common practice that the horns composing an array all have an identical shape. In such a construction, the interval between horn openings is equal to the interval between slots as taken at the bottoms of the horns. When a waveguide for supplying or receiving a signal wave is connected at the bottom of each horn, the interval between such connections is also equal to the interval between horn openings. Thus, the conventional construction has imposed constraints on the positioning of horn openings and waveguides.
In the present embodiment, at least one horn among a plurality of horns disposed side-by-side in one row has a shape which is asymmetric with respect to a plane that is perpendicular to both of the aperture plane of the horn and the E plane. This ensures that the distance between the centers of the openings of two adjacent horns is different from the distance between the centers of two slots communicating with these horns. This allows the positioning of horn openings and waveguides to be more freely designed.
Without being limited to a waffle iron ridge waveguide (WRG) as has been described above, each waveguide according to the present embodiment may alternatively be a hollow waveguide. Hereinafter, examples of using WRGs will be described first, followed by examples of using hollow waveguides.
The antenna array according to the present embodiment includes a conductive member 110 having a first conductive surface 110b on the front side and a second conductive surface 110a on the rear side. The conductive member 110 has a plurality of slots 112 forming a row along a first direction. The first conductive surface 110b of the conductive member 110 is shaped so as to define a plurality of horns 114 respectively communicating with the plurality of slots 112. The respective E planes of the plurality of slots 112 are on the same plane, or on a plurality of planes which are substantially parallel to one another. Herein, “a plurality of planes which are substantially parallel to one another” are not meant to be planes which are strictly parallel to one another. In the present disclosure, any number of planes which constitute angles within ±π/32 with one another are regarded as substantially parallel. This condition may also be expressed as ±5.63 degrees. A plurality of planes which are substantially parallel to one another may also be expressed as “a plurality of planes in uniform orientation”. In the examples from
In the present embodiment, in an E-plane cross section of at least one horn among the plurality of horns 114, a length from one of two intersections between the E plane and the edge of the slot communicating with that horn to one of two intersections between the E plane and the edge of the aperture plane of that horn, this length extending along the inner wall surface of the horn, is longer than a length from the other intersection between the E plane and the edge of the slot to the other intersection between the E plane and the edge of the aperture plane of the horn, this length also extending also along the inner wall surface. In other words, the inner wall surface of the horn has a shape which is asymmetric with respect to a plane that passes through the center of the slot and is perpendicular to the aperture plane and to the E plane.
On the other hand, another horn that is adjacent to the aforementioned horn has an asymmetric or symmetric shape which is different from that of the aforementioned horn. In one example, the center of the opening of one of the two adjacent horns is shifted in the first direction from the slot center, whereas the center of the opening of the other horn is shifted in the opposite direction of the first direction from the slot center. Therefore, regarding these two adjacent horns, an axis that passes through the center of one slot and through the center of the aperture plane of one horn is different from, and not parallel to, an axis that passes through the center of the other slot and through the center of the aperture plane of the other horn. With this structure, it is ensured that the distance between the centers of two adjacent slots is different from the distance between the centers of the openings of the two horns respectively communicating with these slots.
The interval between slots is constrained by the wavelength of an electromagnetic wave propagating in the waveguide. Conventional horn structures have required that the interval between the center of the openings of horns be equal to the interval between the centers of slots. According to the present embodiment, this constraint can be eliminated, thereby permitting freer positioning of constituent elements.
In the example of
In the example of
In the example of
Hereinafter, with reference to
As can be seen from these figures, in the array antenna device according to the present embodiment, all of the slots 112 are at symmetric positions with respect to the port 145U. Moreover, the first conductive surface 110b of the first conductive member 110 is shaped so as to define a plurality of horns 114 each communicating with the respectively corresponding slot 112. As shown in
Each of the plurality of horns 114 has a shape which is asymmetric with respect to a plane which passes through the center of the slot 112 and is orthogonal (e.g., parallel to the XZ plane in the example of
In the present embodiment, in
The waveguide extending between the fourth conductive surface 120b of the second conductive member 120 and the waveguide face 122a of the second waveguide member 122L couples to a waveguide on the fourth conductive member 160 shown in
In the example of
The structural details of the second waveguide member 122L functioning as a 4-port divider, the port 145L, and a rectangular hollow-waveguide 165 will be described later.
In this variant, as shown in
In this variant, the even-numbered rows of horns 114 are shifted with respect to the odd-numbered rows of horns 114, along the direction that the waveguide members 122U extend. The amount of shift is about a half of the distance between the centers of the openings of two adjacent horns 114 along the direction that the waveguide members extend. Adopting such a staggered arrangement allows the direction of arrival of a reception wave to be detected not only with respect to the horizontal direction, but also with respect to the vertical direction.
In this variant, too, the plurality of slots 112 are at symmetric positions with respect to the port 145U. In each row, the distance between the centers of the openings of two adjacent horns is set shorter than the distance between the centers of the pair of slots that are the closest to the port 145U. Among the plurality of horns 114, any horn other than those which are at both ends of each row has a shape which is asymmetric with respect to a plane that passes through the center of the slot 112 and is orthogonal to the direction that the waveguide extends. In this variant, the two horns 114 at both ends of each horn row have shapes which are symmetric with respect to the aforementioned plane, and a line passing through the center of the respective slot 112 at the bottom and the center of the opening of the horn is substantially orthogonal to the second conductive surface 110a. Regarding the other four horns 114, the line passing through the center of the slot 112 at the bottom of the horn 114 and the center of the opening of the horn becomes closer to the port 145U away from the center of the slot 112 (i.e., toward the front surface). Among these four horns 114, the inclination of the aforementioned line is increasingly smaller for horns 114 that are more distant from the port 145U.
The fourth to sixth horns 114D, 114E and 114F have shapes obtained by inverting the first to third horns 114A, 114B and 114C, respectively, with respect to a plane which extends through a midpoint between the first horn 114A and the fourth horn 114D and is perpendicular to the E plane thereof. An axis (shown by a broken line in
As can be seen from
As shown in
As shown in
The inventors have found that an horn antenna array of such a structure can reduce the influence of side lobes at the time of electromagnetic wave radiation, thus enabling satisfactory radiation. Hereinafter, this effect will be described by taking as an example a construction including a single-row antenna array.
For comparison, the inventors have also performed a simulation for a construction in which the six horns 114 all have symmetric shapes as shown in
Although the antenna array according to the present embodiment is illustrated as having six slots 112 and horns 114 in each row, the number of slots 112 and horns 114 in each row may be any number which is two or greater. As for the number of rows, without being limited to five rows, any number which is one or more greater may be adopted.
The first direction, i.e., the direction that the plurality of slots 112 in one row are arrayed, does not need to be a direction which is parallel to the E plane of each slot 112.
The aforementioned antenna array having asymmetric horns is applicable not only to an antenna device in which ridge waveguides are used, but also to an antenna device in which hollow waveguides are used. Hereinafter, examples of such constructions will be described.
The conductive member 110 of the antenna array in this example has four slots 112 and four horns 114. Among the four horns 114, the two horns 114 at both ends have symmetric shapes, whereas the inner two horns 114 have asymmetric shapes. Each horn 114 has a pyramidal shape.
As shown in
Example dimensions for
The conductive members 110 and 190 are fixed to each other by a plurality of bolts 116. By adopting asymmetric shapes for at least some of the plurality of horns 114, it becomes easy to achieve desired radiation characteristics or reception characteristics even in the case where the bolts 116 constrain the structure of the hollow waveguide 192, for example.
The plurality of slots 112 are connected to a hollow waveguide 192 which is composed of conductive members 110 and 190. The bottom face of the conductive member 110 functions also as a part of the longitudinal wall of the hollow waveguide 192.
Example dimensions in this example may be as follows. The distance Hd between the centers of the openings of two adjacent horns 114 may be 3.0 mm (approximately 0.77λ0), for example. In an E-plane cross section of each horn 114, a difference S2 of e.g. 0.39 mm (approximately 0.10λ0) may exist between the shortest distance from one of two intersections between the E plane and the edge of the slot 112 to one of two intersections between the E plane and the edge of the aperture plane of the horn 114 and the shortest distance from the other intersection between the E plane and the edge of the slot 112 to the other intersection between the E plane and the edge of the aperture plane of the horn 114. The width A of the aperture plane of each horn 114 along the first direction may be 2.5 mm (approximately 0.64λ0), for example. The distance L from the bottom of each horn 114 to the aperture plane may be 3.0 mm (approximately 0.77λ0), for example. Different dimensions from these dimensions may also be adopted.
In the above example of using a hollow waveguide, it is not necessary for all slots to be connected to one hollow waveguide. Some of the plurality of slots may be connected to one hollow waveguide, while others may be connected to another hollow waveguide.
Embodiment 3 relates to a technique of suppressing signal wave reflection at the port by adapting the choke structure near the port.
A conventional choke structure, as is disclosed in e.g. Patent Document 1, would include an additional ridge having a length of approximately λr/4 (which hereinafter may be referred to as a “choke ridge”). It has been believed that the length of the choke ridge should not be deviated from λr/4, or the function of the choke structure would be undermined.
However, the inventors have found that even if the choke ridge length is shorter than λr/4, the choke structure may still adequately function, and it may even be preferable for the choke ridge length to be shorter than λr/4 in many cases. More preferably, the choke ridge length is not more than λ0/4. Since λ0 is often smaller by about 10% than λr, λ0/4 is also smaller by about 10% than λr/4. Based on this knowledge, the choke ridge length is chosen to be not more than λ0/4 in the waveguide device according to the present embodiment.
The choke structure according to the present embodiment includes: an electrically-conductive ridge (choke ridge) provided at a position adjacent to a port; and one or more electrically conductive rods provided on the conductive surface with a gap from a farther end of the ridge from the port. The choke ridge may also be considered as a part of the waveguide member as split by the port. The choke ridge length may be set to not less than λ0/16 and not more than λ0/4, for example.
In the present embodiment, a portion of the ridge or the port near the choke structure may be recessed or tapered, thereby being able to suppress signal wave reflection. Hereinafter, with respect to the construction of
The third conductive member 140 according to the present embodiment has a port 145L at a position adjacent to one end of the second waveguide member 122L. A choke structure 150 is provided at a position opposing the one end of the second waveguide member 122L via the port 145L.
The choke structure 150 in the present embodiment includes a first portion 150a adjacent to the port 145L and a second portion 150b adjacent to the first portion 150a. The first portion 150a is composed of a recess in one end of the choke structure 150. This recess makes the interval (distance) from the first portion 150a to the fourth conductive surface 120b of the second conductive member 120 longer, by about λ/4, than the interval (distance) from the second portion 150b to the fourth conductive surface 120b of the second conductive member 120, thus realizing an impedance matching structure. In this example, the interval (distance) from the first portion 150a to the fourth conductive surface 120b of the second conductive member 120 is equal to the interval (distance) from the fifth conductive surface 140a of the third conductive member 140 to the fourth conductive surface 120b of the second conductive member 120.
Since such an impedance matching structure is provided on the choke structure 150 side, when a signal wave passes through the port 145L, unwanted reflection at the port 145L is suppressed. As a result, the signal wave is able to efficiently couple to the waveguide extending between the waveguide face 122a of the waveguide member 122L and the fourth conductive surface 120b.
In the example shown in
The above examples each illustrate an impedance matching structure provided at a port 145L that extends from the fifth conductive surface 140a of the third conductive member 140 on the front side through to the sixth conductive surface 140b on the rear side. Similar structures are also applicable to a port or a slot other than the port 145L. The choke structure 150 according to the present embodiment may be provided near any kind of throughhole, such as a port or a slot. For example, the port 145L shown in
As in these examples, a gap enlargement may be provided for the choke structure by introducing a recess or a taper at the choke ridge, whereby a signal wave passing through the port 145 can be restrained from being reflected near the port 145.
Although the above examples illustrate that the port 145 is provided in the second conductive member 120, the port 145 may instead be provided in the first conductive member 110. The port 145 may be allowed to function as a slot (antenna element).
Given that an electromagnetic wave propagating in the waveguide has a central wavelength of λ0 in free space, the length of the waveguide member end portion 156 along the direction of the waveguide may be set equal to or greater than λ0/16 and less than λ0/4, for example.
In the examples shown in
By providing a gap enlargement as shown in
As shown in
The plurality of T-branching portions 122t include: a first branching portion 122t1 at which the stem 122L0 of the waveguide member 122L branches out into two first branches 122L1; two second branching portions 122t2 at each of which a respective first branch 122L1 branches out into two second branches 122L2; and four third branching portions 122t3 at each of which a respective second branch 122L2 branches out into two third branches 122L3. The eight third branches 122L3 functions as the waveguide terminal sections.
A signal wave which has passed through the port (rectangular hollow-waveguide) 165 shown in
The waveguide member 122L shown in
The aforementioned effect is based on the inventors' finding that, when a dent is provided in a bend, signal wave reflection at the bend is suppressed, but that when a bump is provided on a bend, signal wave reflection at the bend conversely increases. In order to enhance the radiation efficiency of an array antenna, it is preferable to suppress reflection at the bends. However, when suppression of side lobes is a priority, it is effective to purposely cause reflection at the outer bends of the waveguide member 122L in the distribution layer, thus suppressing the amplitude of electromagnetic waves to be radiated from the outer slots, as in the present embodiment, for example.
Without being limited to the above structures, various structures for side lobe reduction may be adopted. For example, without altering the height of the bends 122Lb of at least two outer waveguide terminal sections 122L3 from the reference height (i.e., the height of any site without a dent or a bump), dents may be provided at the bends 122Lb of at least two inner waveguide terminal sections 122L3. Alternatively, without altering the height of the bends 122Lb of at least two inner waveguide terminal sections 122L3 from the reference height, bumps may be provided at the bends 122Lb of at least two outer waveguide terminal sections 122L3. The dent depth or the bump height may be different in all of the bends 122Lb, or may be equal among some of the bends 122Lb.
In the present embodiment, the amplitudes of signal waves that are coupled to the outer ports 145U (see
For purposes other than reducing side lobes, at least one of the plurality of waveguide terminal sections 122L3 may have a shape which is different from the shape of another. The shape of each waveguide terminal section may be designed as appropriate, in accordance with the require performance of the array antenna.
In the present embodiment, the waveguide member 122L in the distribution layer may have an 8-port divider construction, or any other construction such as a 4-port divider, a 16-port divider, or a 32-port divider. In other words, in order to obtain the effects of the present embodiment, the waveguide member 122L may have a construction such that one stem branches into 2N (where N is an integer of 2 or greater) waveguide terminal sections via combinations among a plurality of T-branching portions. In such a construction, the waveguide member having a conductive surface opposing the waveguide member 122L at least has 2N ports opposing 2N waveguide terminal sections. By ensuring that at least one of the 2N waveguide terminal sections has a shape which is different from the shape of another, desired radiation characteristics can be realized in accordance with the purpose. While N=3 in the present embodiment, it may alternatively that N=2 or N≥4.
When N≥3, four waveguide terminal sections that are located central (inner) among the 2N waveguide terminal sections may have a different shape from the shape of at least four waveguide terminal sections that are located outward of the four waveguide terminal sections. For example, the bend shapes of the four waveguide terminal sections that are located central may be dented, while the bend shapes of at least four waveguide terminal sections that are located outward of the four waveguide terminal sections may be bumps, whereby a side lobe reduction effect similar to that of the present embodiment can be obtained.
On the other hand, when N=2, two central waveguide terminal sections among the four waveguide terminal sections may have a different shape from the shape of the two waveguide terminal sections that are located outward of the two waveguide terminal sections. For example, the bend shapes of the two central waveguide terminal sections may be dented, while the bend shapes of the two waveguide terminal sections that are located outward of the two waveguide terminal sections may be bumps, whereby a side lobe reduction effect can be obtained for an array antenna having four rows of slots.
Next, the structure and effects of the impedance transforming sections according to the present embodiment will be described. In the following description, the impedance transforming sections 122i1 and 122i2 may be collectively referred to as the “impedance transforming sections 122i”.
As shown in
In the example shown in
In the waveguide member 122L, the length of a portion of the same height along the waveguide would typically be set to about ¼ of the wavelength of a signal wave within the waveguide; unlike this, however, the present embodiment adopts a value which is distant from such values.
In the present embodiment, among the plurality of impedance transforming sections 122i, the length of a first impedance transforming section 122i1 which is relatively far from the waveguide terminal section 122L3, as taken along the waveguide, is shorter than the length of a second impedance transforming section 122i2 which is relatively close to the waveguide terminal section 122L3, as taken along the waveguide. In the example of
Thus, in the present embodiment, in a direction along the waveguide, the first transforming subsection of the first impedance transforming section 122i1 is shorter than the first transforming subsection of each second impedance transforming section 122i2. Moreover, in a direction along the waveguide, the first transforming subsection (length y1) of the first impedance transforming section 122i1 is shorter than the second transforming subsection (length y2) of the first impedance transforming section 122i1, and the first transforming subsection (length y3) of each second impedance transforming section 122i2 is longer than the second transforming subsection (length y4) of the second impedance transforming section 122i2. Moreover, of the first transforming subsection of the first impedance transforming section 122i1, the end that is closer to the waveguide terminal section 122L3 reaches the branching portion 122t which is the farther from the waveguide terminal sections 122L3; on the other hand, of the first transforming subsection of each second impedance transforming section 122i2, the end that is closer to the waveguide terminal sections 122L3 does not reach the branching portion 122t which is the closer to the waveguide terminal section 122L3. This construction successfully enhances the degree of impedance matching in the branching portion 122t, as compared to a generic impedance transformer in which the lengths of all transforming subsections are set to ¼ of the propagation wavelength.
Although the present embodiment illustrates that the third conductive member 140 (distribution layer) has an 8-port divider construction, the second conductive member 120 (excitation layer) may also have a similar construction. In other words, the plurality of waveguide terminal sections 122L3 may oppose the plurality of slots 112 in the first conductive member 110. Such a construction will control an in-plane distribution of the excitation amplitude of the array antenna, thus reducing propagation losses at the branching portions 122t.
As viewed from the normal direction of the conductive surface 160a of the fourth conductive member 160, the rectangular hollow-waveguide 165L has a rectangular shape that is defined by a pair of longer sides and a pair of shorter sides orthogonal to the longer sides. Herein, a “rectangular shape” is not limited to a strict rectangle. For example, shapes with round corners, and shapes in which at least one of the longer side pair and the shorter side pair is deviated from being parallel by a small angle, are also encompassed within “rectangular shapes”.
One of the pair of longer sides of the rectangular hollow-waveguide 165L is in contact with one end of the waveguide member 122X. The other of the pair of longer sides is in contact with a side face of a choke ridge 122X′, which is a constituent element of the choke structure 150. The choke ridge 122X′ might also be regarded as a portion of the waveguide member 122X as split by the rectangular hollow-waveguide 165L. The dimension of the choke ridge 122X′ along the direction that the waveguide member 122X extends is slightly larger than that of each rod 124X. The choke structure 150 is constituted by the choke ridge 122X′ and several rods 124X along its extension. Note that rods 124X may alternatively serve as the choke ridge 122X′.
The plurality of rods 124X on the fourth conductive member 160 include two or more rows of rods 124X which are arrayed on both sides of the waveguide member 122X in a direction along the waveguide member 122X. Also on both sides of the choke ridge 122X′, two or more rows of rods 124X are provided. In
With such a rectangular hollow-waveguide 165L, when an electronic circuit such as an MMIC and a waveguide are connected, the signal wave energy is restrained from leaking, whereby the performance of the array antenna device can be improved.
This Embodiment 6 and the next Embodiment 7 relate to the size of conductive rods and the period with which they are arranged.
Embodiments 6 and 7 are similar in that each conductive rod has a prismatic shape, and that the period with which the conductive rods are arranged is altered by changing the size of its “polygonal sides”. As used herein, a “polygonal side” is a polygonal side along the X direction or the Y direction in
In the preceding embodiments, the leading end 124a of each conductive rod illustrated in the figures is shown to have a substantially square planar shape. In other words, their aspect ratio is substantially 1 (see, for example,
In the present embodiment and the next Embodiment 7, an artificial magnetic conductor is composed of conductive rods each having a non-square planar shape with an aspect ratio that is not 1. A difference between the present embodiment and the next Embodiment 7 is that: in the present embodiment, the polygonal side of each conductive rod along a direction which is parallel to the direction that an adjacent waveguide member extends (the Y direction) is reduced in size; in the next Embodiment 7, the polygonal side of each conductive rod along a direction which is perpendicular to the direction that an adjacent waveguide member extends (the X direction) is reduced in size. Although the X-direction polygonal side of each conductive rod is increased in size in the present embodiment, this is due to their positional relationship with the adjacent waveguide member.
As described above, by forming rises and falls on the waveguide face of the waveguide member, and varying the distance between the waveguide face and the conductive surface of the opposing conductive member along the waveguide, it is possible to reduce the wavelength of a signal wave which propagates on the waveguide. In addition or in the alternative, the wavelength of a signal wave which propagates on the waveguide can be reduced also by varying the width of the waveguide face along the waveguide. The inventors have examined this with respect to a certain example, which showed that, given a central wavelength λr of a signal wave propagating on a waveguide face without rises and falls, for example, the wavelength λg of a signal wave propagating on a waveguide face with rises and falls was λg=0.61λr. For example, if λr=4.5 mm, it was reduced to λg=2.75 mm.
Thus, the inventors have decided to, rather than determining the interval between conductive rods on the basis of the wavelength λr, change the size of conductive rods in a manner of accounting for the reduced wavelength λg. This makes allows the artificial magnetic conductor to have an improved effect of suppressing leakage of electromagnetic waves (signal waves).
Hereinafter, the construction of the conductive rods according to the present embodiment will be described.
While the present embodiment again relates to the construction of an array antenna device, what will mainly be described below is, with respect to the second conductive member 120 (on which conductive rods and waveguide members are provided) of an array antenna device, the structure and arrangement of the conductive rods. Note that the following description is applicable not only to the second conductive member 120, but also to the third conductive member 140 and/or the fourth conductive member 160. As for those constituent elements of the array antenna device which will not be described here, the foregoing description concerning the array antenna device is to be relied on, because their description is not being repeated. Note that, instead of on the second conductive member 120, the plurality of conductive rods may be provided on the conductive surface of the first conductive member opposing each waveguide member.
As described above, it is in answer to adopting a waveguide face which provides a wavelength reduction effect that the high-density conductive rods are provided in the present embodiment. Therefore, the high-density conductive rods are to be provided adjacent to a waveguide member which provides a wavelength reduction effect of at least a predetermined level or greater. On the other hand, at any position that is not adjacent to such a waveguide member, standard conductive rods are provided rather than high-density conductive rods.
First, the standard conductive rod groups 170b and 171b will be described. For instance, the conductive rods 170b1 and 170b2 included in the standard conductive rod group 170b will be described. The leading ends of the conductive rods 170b1 and 170b2 have square planar shapes, with an aspect ratio of 1. The interval between the conductive rods 170b1 and 170b2 (i.e., the distance of their gap along the Y direction) is designed to be substantially equal to the length of one side of this square.
To give a specific example, each polygonal side of the conductive rods 170b1 and 170b2 may be 0.5 mm, and the interval between the conductive rods may also be 0.5 mm. In other words, regarding the Y direction, the conductive rod group 170b is arranged so that conductive rods having 0.5 mm polygonal sides are disposed in a periodic array at intervals of 0.5 mm.
Next, the high-density conductive rod groups 170a, 171a and 172a will be described. For instance, conductive rods 170a1 and 170a2 included in the high-density conductive rod group 170a will be described. The leading ends 124a of the conductive rods 170a1 and 170a2 have rectangle planar shapes, with an aspect ratio which is not 1. The length of their Y-direction polygonal sides is shorter than the length of the polygonal sides of the conductive rods 170b1 and 170b2. On the other hand, the interval between the conductive rods 170a1 and 170a2 (i.e., the distance of their gap along the Y direction) is equal to the interval between the conductive rods 170b1 and 170b2 in the present embodiment.
To give a specific example, each polygonal side of the conductive rods 170a1 and 170a2 along the Y direction may be 0.325 mm, and the interval between the conductive rods may be 0.5 mm. In other words, regarding the Y direction, the high-density conductive rod group 170a is arranged so that conductive rods having 0.325 mm polygonal sides are disposed in a periodic array at intervals of 0.5 mm.
In a comparison between the period with which the conductive rods in the high-density conductive rod groups 170a, 171a and 172a are arrayed and the period with which the conductive rods in the standard conductive rod groups 170b and 171b are arrayed, it is the latter that is longer. In the above specific example, the latter is 0.175 mm longer per period. Therefore, given a range of the same length, a greater number of conductive rods can be provided in each high-density conductive rod group. Thus, leakage of a signal wave propagate in the waveguide member can be suppressed more effectively.
Hereinafter, the dimension and arrangement of the conductive rods, along the X direction, that compose each high-density conductive rod group will also be described. Attention will be paid to a conductive rod 171a1 in the high-density conductive rod group 171a in
As has been described in “(1) width of the conductive rod” above, the width (i.e., the size along the X direction and along the Y direction) of a conductive rod may be set to be less than λm/2, and more preferably less than λ0/4.
Thus, the inventors have set the size of the conductive rod 171a1 along the X direction to be less than λ0/4. In addition, it is ensured that the distance (i.e., the size of the gap; the same definition will also apply below) between the conductive rod 171a1 and the waveguide member 122L-a1, and the distance between the conductive rod 171a1 and the waveguide member 122L-a2, are greater than those in the standard conductive rod groups.
To give a specific example, the width of the conductive rod 171a1 along the X direction is 0.75 mm (=0.19λ0), which is 0.25 mm longer than that of the conductive rod 170b1. The distance between the conductive rod 171a1 and the waveguide member 122L-a1, and the distance between the conductive rod 171a1 and the waveguide member 122L-a2, are both 0.625 mm (=0.16·λ0)), which is 0.125 mm longer than the distance between the conductive rod 170b1 and the waveguide member 122L-b.
In
In the present embodiment, the period with which the conductive rod groups 170a, 171a and 172a are disposed are arranged along the Y direction (i.e., the distance between the centers of adjacent rods) is equal to ½ of the distance between a port 145a1 in the waveguide member 122L-a1 and a port 145a2 in the waveguide member 122L-a2, as taken along the Y direction. By choosing such a period, even though the ports 145a1 and 145a2 are at different positions along the Y direction, the horizontal portions (lateral portions) of the H-shaped ports 145a1 and 145a2 along the Y direction are aligned with the positions of the respectively adjacent conductive rods 171a along the Y direction. By choosing such relative positioning, the states of electric fields near the ports 145a1 and 145a2 can be made identical. The period with which the conductive rods 170a, 171a and 172a may be arranged along the Y direction in order for this effect to be attained is not limited to ½ of the period with which the port 145a1 and the port 145a2 are disposed along the Y direction. Stated more generally, a dimension which is an integer fraction of 1 (where the integer includes 1) can be selected. In the case where maintaining identical states of electric fields is the purpose, it is not necessary to adopt any waveguide face that provides a wavelength reduction effect.
The preceding embodiments have illustrated, as shown in e.g.
When a plurality of waveguide members are provided, their interval affects the reception performance and/or the transmission performance of the antenna array. For example, the interval between the plurality of waveguide members provided in the excitation layer determines the arraying interval of antenna elements (i.e., the interval between the centers of two adjacent antenna elements). As has already been described, if the interval between the centers of two adjacent antenna elements becomes greater than the wavelength of an electromagnetic wave used, grating lobes will appear in the visible region of the antenna. When the arraying interval between antenna element further increases, the directions of grating lobes will become closer to the direction of the main lobe. This makes it necessary to reduce the arraying interval of the antenna elements, i.e., the interval between waveguide members. Moreover, in order to expand the angular range in which the antenna array is capable of reception, the waveguide members in the excitation layer need to be provided at smaller intervals.
When the interval between waveguide members is reduced, the number of conductive rod rows to be provided therebetween may become restricted. For example, depending on the interval between two adjacent waveguide members, it may only be possible for one row of conductive rods to be provided, which may not achieve adequate electromagnetic isolation between the waveguide faces. This results in a possibility that an electromagnetic wave propagating within a given waveguide may leak out to an adjacent waveguide face.
Accordingly, regarding any conductive rod that is disposed adjacent to a waveguide member, the inventors have decided to reduce the size of its polygonal side extending in a direction perpendicular to the waveguide member (i.e., the X direction), within a plane which is parallel to the waveguide member. This ensures that each waveguide member is surrounded by at least two rows of conductive rods, whereby sufficient electromagnetic isolation between the waveguide faces can be achieved.
Hereinafter, the construction according to the present embodiment will be described.
While the present embodiment again relates to the construction of an array antenna device, what will mainly be described below is, with respect to the second conductive member 120 (on which conductive rods and waveguide members are provided) of an array antenna device, the structure and arrangement of the conductive rods. Note that the following description is applicable not only to the second conductive member 120, but also to the third conductive member 140 and/or the fourth conductive member 160. As for those constituent elements of the array antenna device which will not be described here, the foregoing description concerning the array antenna device is to be relied on, because their description is not being repeated. Note that, instead of on the second conductive member 120, the plurality of conductive rods may be provided on the conductive surface of the first conductive member opposing each waveguide member.
Hereinafter, each conductive rod in the conductive rod groups 180 to 182 will be referred to as a “conductive rod according to the present embodiment”, whereas each conductive rod in each standard conductive rod group 184 will be referred to as a “standard conductive rod”. It will be understood that the conductive rod according to the present embodiment is smaller than the standard conductive rod.
The span from the waveguide member 122L-c to the waveguide member 122L-d may be divided up as follows.
w1: distance from the waveguide member 122L-c to the conductive rod 180a
w2: width of the conductive rod 180a along the X direction
w3: distance from the conductive rod 180a to the conductive rod 180b
w4: width of the conductive rod 180b along the X direction
w5: distance from the conductive rod 180b to the waveguide member 122L-d
The present embodiment conveniently assumes that w2=w4, w1=w5. However, this is not an essential requirement.
As described above, w2 and w4 are shorter than the width of a standard conductive rod along the X direction in the present embodiment. For example, if the width of a standard conductive rod along the X direction is λ0/8, then w2 and w4 may be λ0/16. This allows w3 to be about λ0/8. If w1 and w5 are allowed to be λ0/8, then the interval from the waveguide member 122L-c to the waveguide member 122L-d will be about λ0/2.
On the other hand, on the XY plane, if a standard conductive rod is a square having polygonal sides that are λ0/8 long and the interval between two rows of rods is also λ0/8, then the interval between the two waveguide members is λ0·5/8. Therefore, the interval between the two waveguide members is shorter in the construction of the present embodiment.
The dimension of a conductive rod according to the present embodiment along the Y direction is set to be longer than its dimension along the X direction. Thus, strength of each conductive rod is ensured. However, along the Y direction as well, the dimension of a conductive rod according to the present embodiment can be made shorter than the dimension of a standard conductive rod. This allows the high-density conductive as described in Embodiment 6 to be provided.
Embodiments 6 and 7 above illustrate that conductive rods have prismatic shapes. Alternatively, the conductive rods may have cylindrical shapes. In that case, the radius of each cylinder may be decreased, for example, thus to improve the density with which the conductive rods are disposed in a direction along the waveguide member, or to increase the number of rows of conductive rods to be disposed between mutually adjacent waveguide members. Alternatively, the conductive rods may be composed of elliptic cylinders rather than cylinders, where the longer side and the shorter side as referred to in the above description for a rectangle should read as the major axis and the minor axis of an ellipse, respectively.
(Specific Example of Array Antenna Device)
Thus, illustrative embodiments of the present invention have been described above. Hereinafter, with reference to
The array antenna device 1000 is composed of four conductive members which are layered upon one another. Specifically, in the +Z direction, a fourth conductive member 160, a third conductive member 140, a second conductive member 120, and a first conductive member 110 are layered in this order. The spacing between two opposing conductive members is as described above.
The respective port provided in each conductive member and the respective waveguide in the layer on its rear side (i.e., the −Z direction side) are disposed opposite to each other. For example, the conductive member 140 will be discussed. Between the waveguide face of a waveguide member which is provided on the conductive member 140 and the conductive surface of the conductive member 120 opposing the conductive member 140, a waveguide is created. The waveguide is connected to a port which is provided in the conductive member 140. On the conductive member 160 immediately below the port, a waveguide pertaining to that layer is created at a position opposing the port. This allows a signal wave to propagate through the port to the lower layer. Conversely, a signal wave which is generated by an electronic circuit 310, e.g., MMIC, (
As shown in
As the antenna A2, the array antenna shown in
As the antenna A3, an array antenna including a plurality of horns 114 disposed side-by-side in each row, as in the construction shown in
Note that portion C surrounded by a broken circle in
<Variants>
Next, other variants of the waveguide member 122, the conductive members 110 and 120, and the conductive rod 124 will be described.
The dielectric layer on the outermost surface will allow losses to be increased in the electromagnetic wave propagating through the WRG waveguide, but is able to protect the conductive surfaces 110a and 120a (which are electrically conductive) from corrosion. It also prevents influences of a DC voltage, or an AC voltage of such a low frequency that it is not capable of propagation on certain WRG waveguides.
The waveguide device and antenna device according to the present embodiment can be suitably used in a radar device to be incorporated in moving entities such as vehicles, marine vessels, aircraft, robots, or the like (hereinafter simply referred to as a “radar”), or a radar system, for example. A radar would include an antenna device according to an embodiment of the present disclosure and a microwave integrated circuit that is connected to the antenna device. A radar system would include the radar device and a signal processing circuit that is connected to the microwave integrated circuit of the radar device. An antenna device according to the present embodiment includes a WRG structure which permits downsizing, and thus allows the area of the face on which antenna elements are arrayed to be reduced, as compared to a construction in which a conventional hollow waveguide is used. Therefore, a radar system incorporating the antenna device can be easily mounted in a narrow place such as a face of a rearview mirror in a vehicle that is opposite to its specular surface, or a small-sized moving entity such as a UAV (an Unmanned Aerial Vehicle, a so-called drone). Note that, without being limited to the implementation where it is mounted in a vehicle, a radar system may be used while being fixed on the road or a building, for example.
A slot array antenna according to an embodiment of the present disclosure can also be used in a wireless communication system. Such a wireless communication system would include a slot array antenna according to any of the above embodiments and a communication circuit (a transmission circuit or a reception circuit). Details of exemplary applications to wireless communication systems will be described later.
A slot array antenna according to an embodiment of the present disclosure can further be used as an antenna in an indoor positioning system (IPS). An indoor positioning system is able to identify the position of a moving entity, such as a person or an automated guided vehicle (AGV), that is in a building. An array antenna can also be used as a radio wave transmitter (beacon) for use in a system which provides information to an information terminal device (e.g., a smartphone) that is carried by a person who has visited a store or any other facility. In such a system, once every several seconds, a beacon may radiate an electromagnetic wave carrying an ID or other information superposed thereon, for example. When the information terminal device receives this electromagnetic wave, the information terminal device transmits the received information to a remote server computer via telecommunication lines. Based on the information that has been received from the information terminal device, the server computer identifies the position of that information terminal device, and provides information which is associated with that position (e.g., product information or a coupon) to the information terminal device.
The present specification employs the term “artificial magnetic conductor” in describing the technique according to the present disclosure, this being in line with what is set forth in a paper by one of the inventors Kirino (Non-Patent Document 1) as well as a paper by Kildal et al., who published a study directed to related subject matter around the same time. However, it has been found through a study by the inventors that the invention according to the present disclosure does not necessarily require an “artificial magnetic conductor” under its conventional definition. That is, while a periodic structure has been believed to be a requirement for an artificial magnetic conductor, the invention according to the present disclosure does not necessary require a periodic structure in order to be practiced.
The artificial magnetic conductor that is described in the embodiments of the present disclosure consists of rows of conductive rods, for example. In order to prevent electromagnetic waves from leaking away from the waveguide face, it has been believed essential that there exist at least two rows of conductive rods on one side of the waveguide member(s), such rows of conductive rods extending along the waveguide member(s) (ridge(s)). The reason is that it takes at least two rows of conductive rods for them to have a “period”. However, according to a study by the inventors, even when only one row of conductive rods, or only one conductive rod, exists between two waveguide members that extend in parallel to each other, the intensity of a signal that leaks from one waveguide member to the other waveguide member can be suppressed to −10 dB or less, which is a practically sufficient value in many applications. The reason why such a sufficient level of separation is achieved with only an imperfect periodic structure is so far unclear. However, in view of this fact, in the present disclosure, the conventional notion of “artificial magnetic conductor” is extended so that the term also encompasses a structure including only one row of conductive rods, or only one conductive rod.
<Application Example 1: Onboard Radar System>
Next, as an Application Example of utilizing the above-described array antenna device, an instance of an onboard radar system including an array antenna device will be described. A transmission wave used in an onboard radar system may have a frequency of e.g. 76 gigahertz (GHz) band, which will have a wavelength λ0 of about 4 mm in free space.
In safety technology of automobiles, e.g., collision avoidance systems or automated driving, it is particularly essential to identify one or more vehicles (targets) that are traveling ahead of the driver's vehicle. As a method of identifying vehicles, techniques of estimating the directions of arriving waves by using a radar system have been under development.
The onboard radar system 510 of this Application Example includes a slot array antenna device according to the any of the above embodiments. This Application Example is arranged so that the direction that each of the plurality of waveguide members extends coincides with the vertical direction, and that the direction in which the plurality of waveguide members are arrayed (with respect to one another) coincides with the horizontal direction. As a result, the lateral dimension of the plurality of slots as viewed from the front can be reduced. Exemplary dimensions of an antenna device including the above array antenna device may be 60 mm (wide)×30 mm (long)×10 mm (deep). It will be appreciated that this is a very small size for a millimeter wave radar system of the 76 GHz band.
Note that many a conventional onboard radar system is provided outside the vehicle, e.g., at the tip of the front nose. The reason is that the onboard radar system is relatively large in size, and thus is difficult to be provided within the vehicle as in the present disclosure. The onboard radar system 510 of this Application Example may be installed within the vehicle as described above, but may instead be mounted at the tip of the front nose. Since the footprint of the onboard radar system on the front nose is reduced, other parts can be more easily placed.
The Application Example allows the interval between a plurality of waveguide members (ridges) that are used in the transmission antenna to be narrow, which also narrows the interval between a plurality of slots to be provided opposite from a number of adjacent waveguide members. This reduces the influences of grating lobes. For example, when the interval between the centers of two laterally adjacent slots is shorter than the free-space wavelength λ0 of the transmission wave (i.e., less than about 4 mm), no grating lobes will occur frontward. As a result, influences of grating lobes are reduced. Note that grating lobes will occur when the interval at which the antenna elements are arrayed is greater than a half of the wavelength of an electromagnetic wave. If the interval at which the antenna elements are arrayed is less than the wavelength, no grating lobes will occur frontward. Therefore, in the case where no beam steering is performed to impart phase differences among the radio waves radiated from the respective antenna elements composing an array antenna, grating lobes will exert substantially no influences so long as the interval at which the antenna elements are arrayed is smaller than the wavelength. By adjusting the array factor of the transmission antenna, the directivity of the transmission antenna can be adjusted. A phase shifter may be provided so as to be able to individually adjust the phases of electromagnetic waves that are transmitted on plural waveguide members. In this case, in order to avoid the influences of grating lobes, it is preferable that the interval between antenna elements is less than a half of the free-space wavelength λo of the transmission wave. By providing a phase shifter, the directivity of the transmission antenna can be changed in any desired direction. Since the construction of a phase shifter is well-known, description thereof will be omitted.
A reception antenna according to the Application Example is able to reduce reception of reflected waves associated with grating lobes, thereby being able to improve the precision of the below-described processing.
Hereinafter, an example of a reception process will be described.
The array antenna device AA receives plural arriving waves that simultaneously impinge at various angles. Some of the plural arriving waves may be arriving waves which have been radiated from the transmission antenna of the same onboard radar system 510 and reflected by a target(s). Furthermore, some of the plural arriving waves may be direct or indirect arriving waves that have been radiated from other vehicles.
The incident angle of each arriving wave (i.e., an angle representing its direction of arrival) is an angle with respect to the broadside B of the array antenna device AA. The incident angle of an arriving wave represents an angle with respect to a direction which is perpendicular to the direction of the line along which antenna elements are arrayed.
Now, consider a kth arriving wave. Where K arriving waves are impinging on the array antenna device from K targets existing at different azimuths, a “kth arriving wave” means an arriving wave which is identified by an incident angle θk.
S=[s1,s2, . . . ,sM]T (Math. 1)
In the above, sm (where m is an integer from 1 to M; the same will also be true hereinbelow) is the value of a signal which is received by an Mth antenna element. The superscript T means transposition. S is a column vector. The column vector S is defined by a product of multiplication between a direction vector (referred to as a steering vector or a mode vector) as determined by the construction of the array antenna device and a complex vector representing a signal from each target (also referred to as a wave source or a signal source). When the number of wave sources is K, the waves of signals arriving at each individual antenna element from the respective K wave sources are linearly superposed. In this state, sm can be expressed by Math. 2.
In Math. 2, ak, θk and ϕk respectively denote the amplitude, incident angle, and initial phase of the kth arriving wave. Moreover, λ denotes the wavelength of an arriving wave, and j is an imaginary unit.
As will be understood from Math. 2, sm is expressed as a complex number consisting of a real part (Re) and an imaginary part (Im).
When this is further generalized by taking noise (internal noise or thermal noise) into consideration, the array reception signal X can be expressed as Math. 3.
X=S+N (Math. 3)
N is a vector expression of noise.
The signal processing circuit generates a spatial covariance matrix Rxx (Math. 4) of arriving waves by using the array reception signal X expressed by Math. 3, and further determines eigenvalues of the spatial covariance matrix Rxx.
In the above, the superscript H means complex conjugate transposition (Hermitian conjugate).
Among the eigenvalues, the number of eigenvalues which have values equal to or greater than a predetermined value that is defined based on thermal noise (signal space eigenvalues) corresponds to the number of arriving waves. Then, angles that produce the highest likelihood as to the directions of arrival of reflected waves (i.e. maximum likelihood) are calculated, whereby the number of targets and the angles at which the respective targets are present can be identified. This process is known as a maximum likelihood estimation technique.
Next, see
The array antenna device AA includes a plurality of antenna elements, each of which outputs a reception signal in response to one or plural arriving waves. As mentioned earlier, the array antenna device AA is capable of radiating a millimeter wave of a high frequency. Note that, without being limited to the array antenna device according to any of the above embodiments, the array antenna device AA may be any other array antenna device that suitably performs reception.
In the radar system 510, the array antenna device AA needs to be attached to the vehicle, while at least some of the functions of the radar signal processing apparatus 530 may be implemented by a computer 550 and a database 552 which are provided externally to the vehicle travel controlling apparatus 600 (e.g., outside of the driver's vehicle). In that case, the portions of the radar signal processing apparatus 530 that are located within the vehicle may be perpetually or occasionally connected to the computer 550 and database 552 external to the vehicle so that bidirectional communications of signal or data are possible. The communications are to be performed via a communication device 540 of the vehicle and a commonly-available communications network.
The database 552 may store a program which defines various signal processing algorithms. The content of the data and program needed for the operation of the radar system 510 may be externally updated via the communication device 540. Thus, at least some of the functions of the radar system 510 can be realized externally to the driver's vehicle (which is inclusive of the interior of another vehicle), by a cloud computing technique. Therefore, an “onboard” radar system in the meaning of the present disclosure does not require that all of its constituent elements be mounted within the (driver's) vehicle. However, for simplicity, the present application will describe an implementation in which all constituent elements according to the present disclosure are mounted in a single vehicle (i.e., the driver's vehicle), unless otherwise specified.
The radar signal processing apparatus 530 includes a signal processing circuit 560. The signal processing circuit 560 directly or indirectly receives reception signals from the array antenna device AA, and inputs the reception signals, or a secondary signal(s) which has been generated from the reception signals, to an arriving wave estimation unit AU. A part or a whole of the circuit (not shown) which generates a secondary signal(s) from the reception signals does not need to be provided inside of the signal processing circuit 560. A part or a whole of such a circuit (preprocessing circuit) may be provided between the array antenna device AA and the radar signal processing apparatus 530.
The signal processing circuit 560 is configured to perform computation by using the reception signals or secondary signal(s), and output a signal indicating the number of arriving waves. As used herein, a “signal indicating the number of arriving waves” can be said to be a signal indicating the number of preceding vehicles (which may be one preceding vehicle or plural preceding vehicles) ahead of the driver's vehicle.
The signal processing circuit 560 may be configured to execute various signal processing which is executable by known radar signal processing apparatuses. For example, the signal processing circuit 560 may be configured to execute “super-resolution algorithms” such as the MUSIC method, the ESPRIT method, or the SAGE method, or other algorithms for direction-of-arrival estimation of relatively low resolution.
The arriving wave estimation unit AU shown in FIG. estimates an angle representing the azimuth of each arriving wave by an arbitrary algorithm for direction-of-arrival estimation, and outputs a signal indicating the estimation result. The signal processing circuit 560 estimates the distance to each target as a wave source of an arriving wave, the relative velocity of the target, and the azimuth of the target by using a known algorithm which is executed by the arriving wave estimation unit AU, and output a signal indicating the estimation result.
In the present disclosure, the term “signal processing circuit” is not limited to a single circuit, but encompasses any implementation in which a combination of plural circuits is conceptually regarded as a single functional part. The signal processing circuit 560 may be realized by one or more System-on-Chips (SoCs). For example, a part or a whole of the signal processing circuit 560 may be an FPGA (Field-Programmable Gate Array), which is a programmable logic device (PLD). In that case, the signal processing circuit 560 includes a plurality of computation elements (e.g., general-purpose logics and multipliers) and a plurality of memory elements (e.g., look-up tables or memory blocks). Alternatively, the signal processing circuit 560 may be a set of a general-purpose processor(s) and a main memory device(s). The signal processing circuit 560 may be a circuit which includes a processor core(s) and a memory device(s). These may function as the signal processing circuit 560.
The travel assistance electronic control apparatus 520 is configured to provide travel assistance for the vehicle based on various signals which are output from the radar signal processing apparatus 530. The travel assistance electronic control apparatus 520 instructs various electronic control units to fulfill predetermined functions, e.g., a function of issuing an alarm to prompt the driver to make a braking operation when the distance to a preceding vehicle (vehicular gap) has become shorter than a predefined value; a function of controlling the brakes; and a function of controlling the accelerator. For example, in the case of an operation mode which performs adaptive cruise control of the driver's vehicle, the travel assistance electronic control apparatus 520 sends predetermined signals to various electronic control units (not shown) and actuators, to maintain the distance of the driver's vehicle to a preceding vehicle at a predefined value, or maintain the traveling velocity of the driver's vehicle at a predefined value.
In the case of the MUSIC method, the signal processing circuit 560 determines eigenvalues of the spatial covariance matrix, and, as a signal indicating the number of arriving waves, outputs a signal indicating the number of those eigenvalues (“signal space eigenvalues”) which are greater than a predetermined value (thermal noise power) that is defined based on thermal noise.
Next, see
At least one of the transmission antenna Tx and the reception antenna Rx has the aforementioned waveguide structure. The transmission antenna Tx radiates a transmission wave, which may be a millimeter wave, for example. The reception antenna Rx that is dedicated to reception only outputs a reception signal in response to one or plural arriving waves (e.g., a millimeter wave(s)).
A transmission/reception circuit 580 sends a transmission signal for a transmission wave to the transmission antenna Tx, and performs “preprocessing” for reception signals of reception waves received at the reception antenna Rx. A part or a whole of the preprocessing may be performed by the signal processing circuit 560 in the radar signal processing apparatus 530. A typical example of preprocessing to be performed by the transmission/reception circuit 580 may be generating a beat signal from a reception signal, and converting a reception signal of analog format into a reception signal of digital format.
Note that the radar system according to the present disclosure may, without being limited to the implementation where it is mounted in the driver's vehicle, be used while being fixed on the road or a building.
Next, an example of a more specific construction of the vehicle travel controlling apparatus 600 will be described.
The onboard camera system 700 includes an onboard camera 710 which is mounted in a vehicle, and an image processing circuit 720 which processes an image or video that is acquired by the onboard camera 710.
The vehicle travel controlling apparatus 600 of this Application Example includes an object detection apparatus 570 which is connected to the array antenna device AA and the onboard camera 710, and a travel assistance electronic control apparatus 520 which is connected to the object detection apparatus 570. The object detection apparatus 570 includes a transmission/reception circuit 580 and an image processing circuit 720, in addition to the above-described radar signal processing apparatus 530 (including the signal processing circuit 560). The object detection apparatus 570 detects a target on the road or near the road, by using not only the information which is obtained by the radar system 510 but also the information which is obtained by the image processing circuit 720. For example, while the driver's vehicle is traveling in one of two or more lanes of the same direction, the image processing circuit 720 can distinguish which lane the driver's vehicle is traveling in, and supply that result of distinction to the signal processing circuit 560. When the number and azimuth(s) of preceding vehicles are to be recognized by using a predetermined algorithm for direction-of-arrival estimation (e.g., the MUSIC method), the signal processing circuit 560 is able to provide more reliable information concerning a spatial distribution of preceding vehicles by referring to the information from the image processing circuit 720.
Note that the onboard camera system 700 is an example of a means for identifying which lane the driver's vehicle is traveling in. The lane position of the driver's vehicle may be identified by any other means. For example, by utilizing an ultra-wide band (UWB) technique, it is possible to identify which one of a plurality of lanes the driver's vehicle is traveling in. It is widely known that the ultra-wide band technique is applicable to position measurement and/or radar. Using the ultra-wide band technique enhances the range resolution of the radar, so that, even when a large number of vehicles exist ahead, each individual target can be detected with distinction, based on differences in distance. This makes it possible to identify distance from a guardrail on the road shoulder, or from the median strip. The width of each lane is predefined based on each country's law or the like. By using such information, it becomes possible to identify where the lane in which the driver's vehicle is currently traveling is. Note that the ultra-wide band technique is an example. A radio wave based on any other wireless technique may be used. Moreover, LIDAR (Light Detection and Ranging) may be used together with a radar. LIDAR is sometimes called “laser radar”.
The array antenna device AA may be a generic millimeter wave array antenna device for onboard use. The transmission antenna Tx in this Application Example radiates a millimeter wave as a transmission wave ahead of the vehicle. A portion of the transmission wave is reflected off a target which is typically a preceding vehicle, whereby a reflected wave occurs from the target being a wave source. A portion of the reflected wave reaches the array antenna device (reception antenna) AA as an arriving wave. Each of the plurality of antenna elements of the array antenna device AA outputs a reception signal in response to one or plural arriving waves. In the case where the number of targets functioning as wave sources of reflected waves is K (where K is an integer of one or more), the number of arriving waves is K, but this number K of arriving waves is not known beforehand.
The example of
The signal processing circuit 560 receives and processes the reception signals which have been received by the reception antenna Rx and subjected to preprocessing by the transmission/reception circuit 580. This process encompasses inputting the reception signals to the arriving wave estimation unit AU, or alternatively, generating a secondary signal(s) from the reception signals and inputting the secondary signal(s) to the arriving wave estimation unit AU.
In the example of
As shown in
In the array antenna device AA, the antenna elements 111 to 11M are arranged in a linear array or a two-dimensional array at fixed intervals, for example. Each arriving wave will impinge on the array antenna device AA from a direction at an angle θ with respect to the normal of the plane in which the antenna elements 111 to 11M are arrayed. Thus, the direction of arrival of an arriving wave is defined by this angle θ.
When an arriving wave from one target impinges on the array antenna device AA, this approximates to a plane wave impinging on the antenna elements 111 to 11M from azimuths of the same angle θ. When K arriving waves impinge on the array antenna device AA from K targets with different azimuths, the individual arriving waves can be identified in terms of respectively different angles θ1 to θK.
As shown in
The transmission/reception circuit 580 includes a triangular wave generation circuit 581, a VCO (voltage controlled oscillator) 582, a distributor 583, mixers 584, filters 585, a switch 586, an A/D converter 587, and a controller 588. Although the radar system in this Application Example is configured to perform transmission and reception of millimeter waves by the FMCW method, the radar system of the present disclosure is not limited to this method. The transmission/reception circuit 580 is configured to generate a beat signal based on a reception signal from the array antenna device AA and a transmission signal from the transmission antenna Tx.
The signal processing circuit 560 includes a distance detection section 533, a velocity detection section 534, and an azimuth detection section 536. The signal processing circuit 560 is configured to process a signal from the A/D converter 587 in the transmission/reception circuit 580, and output signals respectively indicating the detected distance to the target, the relative velocity of the target, and the azimuth of the target.
First, the construction and operation of the transmission/reception circuit 580 will be described in detail.
The triangular wave generation circuit 581 generates a triangular wave signal, and supplies it to the VCO 582. The VCO 582 outputs a transmission signal having a frequency as modulated based on the triangular wave signal.
In addition to the transmission signal,
When the reception signal and the transmission signal are mixed, a beat signal is generated based on their frequency difference. The frequency of this beat signal (beat frequency) differs between a period in which the transmission signal increases in frequency (ascent) and a period in which the transmission signal decreases in frequency (descent). Once a beat frequency for each period is determined, based on such beat frequencies, the distance to the target and the relative velocity of the target are calculated.
In the example shown in
The switch 586 performs switching in response to a sampling signal which is input from the controller 588. The controller 588 may be composed of a microcomputer, for example. Based on a computer program which is stored in a memory such as a ROM, the controller 588 controls the entire transmission/reception circuit 580. The controller 588 does not need to be provided inside the transmission/reception circuit 580, but may be provided inside the signal processing circuit 560. In other words, the transmission/reception circuit 580 may operate in accordance with a control signal from the signal processing circuit 560. Alternatively, some or all of the functions of the controller 588 may be realized by a central processing unit which controls the entire transmission/reception circuit 580 and signal processing circuit 560.
The beat signals on the channels Ch1 to ChM having passed through the respective filters 585 are consecutively supplied to the A/D converter 587 via the switch 586. In synchronization with the sampling signal, the A/D converter 587 converts the beat signals on the channels Ch1 to ChM, which are input from the switch 586, into digital signals.
Hereinafter, the construction and operation of the signal processing circuit 560 will be described in detail. In this Application Example, the distance to the target and the relative velocity of the target are estimated by the FMCW method. Without being limited to the FMCW method as described below, the radar system can also be implemented by using other methods, e.g., 2 frequency CW and spread spectrum methods.
In the example shown in
The signal processing circuit 560 in this Application Example is configured to estimate the position information of a preceding vehicle by using each beat signal converted into a digital signal as a secondary signal of the reception signal, and output a signal indicating the estimation result. Hereinafter, the construction and operation of the signal processing circuit 560 in this Application Example will be described in detail.
For each of the channels Ch1 to ChM, the memory 531 in the signal processing circuit 560 stores a digital signal which is output from the A/D converter 587. The memory 531 may be composed of a generic storage medium such as a semiconductor memory or a hard disk and/or an optical disk.
The reception intensity calculation section 532 applies Fourier transform to the respective beat signals for the channels Ch1 to ChM (shown in the lower graph of
In the case where there is one target, i.e., one preceding vehicle, as shown in
From the signal intensities of beat frequencies, the reception intensity calculation section 532 detects any signal intensity that exceeds a predefined value (threshold value), thus determining the presence of a target. Upon detecting a signal intensity peak, the reception intensity calculation section 532 outputs the beat frequencies (fu, fd) of the peak values to the distance detection section 533 and the velocity detection section 534 as the frequencies of the object of interest. The reception intensity calculation section 532 outputs information indicating the frequency modulation width Δf to the distance detection section 533, and outputs information indicating the center frequency f0 to the velocity detection section 534.
In the case where signal intensity peaks corresponding to plural targets are detected, the reception intensity calculation section 532 find associations between the ascents peak values and the descent peak values based on predefined conditions. Peaks which are determined as belonging to signals from the same target are given the same number, and thus are fed to the distance detection section 533 and the velocity detection section 534.
When there are plural targets, after the Fourier transform, as many peaks as there are targets will appear in the ascent portions and the descent portions of the beat signal. In proportion to the distance between the radar and a target, the reception signal will become more delayed and the reception signal in
Based on the beat frequencies fu and fd which are input from the reception intensity calculation section 532, the distance detection section 533 calculates a distance R through the equation below, and supplies it to the target link processing section 537.
R={c·T/(2·Δf)}·{(fu+fd)/2}
Moreover, based on the beat frequencies fu and fd being input from the reception intensity calculation section 532, the velocity detection section 534 calculates a relative velocity V through the equation below, and supplies it to the target link processing section 537.
V={c/(2·f0)}·{(fu−fd)/2}
In the equation which calculates the distance R and the relative velocity V, c is velocity of light, and T is the modulation period.
Note that the lower limit resolution of distance R is expressed as c/(2Δf). Therefore, as Δf increases, the resolution of distance R increases. In the case where the frequency f0 is in the 76 GHz band, when Δf is set on the order of 660 megahertz (MHz), the resolution of distance R will be on the order of 0.23 meters (m), for example. Therefore, if two preceding vehicles are traveling abreast of each other, it may be difficult with the FMCW method to identify whether there is one vehicle or two vehicles. In such a case, it might be possible to run an algorithm for direction-of-arrival estimation that has an extremely high angular resolution to separate between the azimuths of the two preceding vehicles and enable detection.
By utilizing phase differences between signals from the antenna elements 111, 112, . . . , 11M, the DBF processing section 535 allows the incoming complex data corresponding to the respective antenna elements, which has been Fourier transformed with respect to the time axis, to be Fourier transformed with respect to the direction in which the antenna elements are arrayed. Then, the DBF processing section 535 calculates spatial complex number data indicating the spectrum intensity for each angular channel as determined by the angular resolution, and outputs it to the azimuth detection section 536 for the respective beat frequencies.
The azimuth detection section 536 is provided for the purpose of estimating the azimuth of a preceding vehicle. Among the values of spatial complex number data that has been calculated for the respective beat frequencies, the azimuth detection section 536 chooses an angle θ that takes the largest value, and outputs it to the target link processing section 537 as the azimuth at which an object of interest exists.
Note that the method of estimating the angle θ indicating the direction of arrival of an arriving wave is not limited to this example. Various algorithms for direction-of-arrival estimation that have been mentioned earlier can be employed.
The target link processing section 537 calculates absolute values of the differences between the respective values of distance, relative velocity, and azimuth of the object of interest as calculated in the current cycle and the respective values of distance, relative velocity, and azimuth of the object of interest as calculated 1 cycle before, which are read from the memory 531. Then, if the absolute value of each difference is smaller than a value which is defined for the respective value, the target link processing section 537 determines that the target that was detected 1 cycle before and the target detected in the current cycle are an identical target. In that case, the target link processing section 537 increments the count of target link processes, which is read from the memory 531, by one.
If the absolute value of a difference is greater than predetermined, the target link processing section 537 determines that a new object of interest has been detected. The target link processing section 537 stores the respective values of distance, relative velocity, and azimuth of the object of interest as calculated in the current cycle and also the count of target link processes for that object of interest to the memory 531.
In the signal processing circuit 560, the distance to the object of interest and its relative velocity can be detected by using a spectrum which is obtained through a frequency analysis of beat signals, which are signals generated based on received reflected waves.
The matrix generation section 538 generates a spatial covariance matrix by using the respective beat signals for the channels Ch1 to ChM (lower graph in
When a plurality of signal intensity peaks corresponding to plural objects of interest have been detected, the reception intensity calculation section 532 numbers the peak values respectively in the ascent portion and in the descent portion, beginning from those with smaller frequencies first, and output them to the target output processing section 539. In the ascent and descent portions, peaks of any identical number correspond to the same object of interest. The identification numbers are to be regarded as the numbers assigned to the objects of interest. For simplicity of illustration, a leader line from the reception intensity calculation section 532 to the target output processing section 539 is conveniently omitted from
When the object of interest is a structure ahead, the target output processing section 539 outputs the identification number of that object of interest as indicating a target. When receiving results of determination concerning plural objects of interest, such that all of them are structures ahead, the target output processing section 539 outputs the identification number of an object of interest that is in the lane of the driver's vehicle as the object position information indicating where a target is. Moreover, When receiving results of determination concerning plural objects of interest, such that all of them are structures ahead and that two or more objects of interest are in the lane of the driver's vehicle, the target output processing section 539 outputs the identification number of an object of interest that is associated with the largest count of target being read from the link processes memory 531 as the object position information indicating where a target is.
Referring back to
The selection circuit 596 selectively feeds position information which is received from the signal processing circuit 560 or the image processing circuit 720 to the travel assistance electronic control apparatus 520. For example, the selection circuit 596 compares a first distance, i.e., the distance from the driver's vehicle to a detected object as contained in the object position information from the signal processing circuit 560, against a second distance, i.e., the distance from the driver's vehicle to the detected object as contained in the object position information from the image processing circuit 720, and determines which is closer to the driver's vehicle. For example, based on the result of determination, the selection circuit 596 may select the object position information which indicates a closer distance to the driver's vehicle, and output it to the travel assistance electronic control apparatus 520. If the result of determination indicates the first distance and the second distance to be of the same value, the selection circuit 596 may output either one, or both of them, to the travel assistance electronic control apparatus 520.
If information indicating that there is no prospective target is input from the reception intensity calculation section 532, the target output processing section 539 (
Based on predefined conditions, the travel assistance electronic control apparatus 520 having received the position information of a preceding object from the object detection apparatus 570 performs control to make the operation safer or easier for the driver who is driving the driver's vehicle, in accordance with the distance and size indicated by the object position information, the velocity of the driver's vehicle, road surface conditions such as rainfall, snowfall or clear weather, or other conditions. For example, if the object position information indicates that no object has been detected, the travel assistance electronic control apparatus 520 may send a control signal to an accelerator control circuit 526 to increase speed up to a predefined velocity, thereby controlling the accelerator control circuit 526 to make an operation that is equivalent to stepping on the accelerator pedal.
In the case where the object position information indicates that an object has been detected, if it is found to be at a predetermined distance from the driver's vehicle, the travel assistance electronic control apparatus 520 controls the brakes via a brake control circuit 524 through a brake-by-wire construction or the like. In other words, it makes an operation of decreasing the velocity to maintain a constant vehicular gap. Upon receiving the object position information, the travel assistance electronic control apparatus 520 sends a control signal to an alarm control circuit 522 so as to control lamp illumination or control audio through a loudspeaker which is provided within the vehicle, so that the driver is informed of the nearing of a preceding object. Upon receiving object position information including a spatial distribution of preceding vehicles, the travel assistance electronic control apparatus 520 may, if the traveling velocity is within a predefined range, automatically make the steering wheel easier to operate to the right or left, or control the hydraulic pressure on the steering wheel side so as to force a change in the direction of the wheels, thereby providing assistance in collision avoidance with respect to the preceding object.
The object detection apparatus 570 may be arranged so that, if a piece of object position information which was being continuously detected by the selection circuit 596 for a while in the previous detection cycle but which is not detected in the current detection cycle becomes associated with a piece of object position information from a camera-detected video indicating a preceding object, then continued tracking is chosen, and object position information from the signal processing circuit 560 is output with priority.
An exemplary specific construction and an exemplary operation for the selection circuit 596 to make a selection between the outputs from the signal processing circuit 560 and the image processing circuit 720 are disclosed in the specification of U.S. Pat. No. 8,446,312, the specification of U.S. Pat. No. 8,730,096, and the specification of U.S. Pat. No. 8,730,099. The entire disclosure thereof is incorporated herein by reference.
[First Variant]
In the radar system for onboard use of the above Application Example, the (sweep) condition for a single instance of FMCW (Frequency Modulated Continuous Wave) frequency modulation, i.e., a time span required for such a modulation (sweep time), is e.g. 1 millisecond, although the sweep time could be shortened to about 100 microseconds.
However, in order to realize such a rapid sweep condition, not only the constituent elements involved in the radiation of a transmission wave, but also the constituent elements involved in the reception under that sweep condition must also be able to rapidly operate. For example, an A/D converter 587 (
In the present variant, a relative velocity with respect to a target is calculated without utilizing any Doppler shift-based frequency component. In this variant, the sweep time is Tm=100 microseconds, which is very short. The lowest frequency of a detectable beat signal, which is 1/Tm, equals 10 kHz in this case. This would correspond to a Doppler shift of a reflected wave from a target which has a relative velocity of approximately 20 m/second. In other words, so long as one relies on a Doppler shift, it would be impossible to detect relative velocities that are equal to or smaller than this. Thus, a method of calculation which is different from a Doppler shift-based method of calculation is preferably adopted.
As an example, this variant illustrates a process that utilizes a signal (upbeat signal) representing a difference between a transmission wave and a reception wave which is obtained in an upbeat (ascent) portion where the transmission wave increases in frequency. A single sweep time of FMCW is 100 microseconds, and its waveform is a sawtooth shape which is composed only of an upbeat portion. In other words, in this variant, the signal wave which is generated by the triangular wave/CW wave generation circuit 581 has a sawtooth shape. The sweep width in frequency is 500 MHz. Since no peaks are to be utilized that are associated with Doppler shifts, the process is not one that generates an upbeat signal and a downbeat signal to utilize the peaks of both, but will rely on only one of such signals. Although a case of utilizing an upbeat signal will be illustrated herein, a similar process can also be performed by using a downbeat signal.
The A/D converter 587 (
In this variant, 128 upbeat signals are transmitted/received in series, for each of which some several hundred pieces of sampling data are obtained. The number of upbeat signals is not limited to 128. It may be 256, or 8. An arbitrary number may be selected depending on the purpose.
The resultant sampling data is stored to the memory 531. The reception intensity calculation section 532 applies a two-dimensional fast Fourier transform (FFT) to the sampling data. Specifically, first, for each of the sampling data pieces that have been obtained through a single sweep, a first FFT process (frequency analysis process) is performed to generate a power spectrum. Next, the velocity detection section 534 performs a second FFT process for the processing results that have been collected from all sweeps.
When the reflected waves are from the same target, peak components in the power spectrum to be detected in each sweep period will be of the same frequency. On the other hand, for different targets, the peak components will differ in frequency. Through the first FFT process, plural targets that are located at different distances can be separated.
In the case where a relative velocity with respect to a target is non-zero, the phase of the upbeat signal changes slightly from sweep to sweep. In other words, through the second FFT process, a power spectrum whose elements are the data of frequency components that are associated with such phase changes will be obtained for the respective results of the first FFT process.
The reception intensity calculation section 532 extracts peak values in the second power spectrum above, and sends them to the velocity detection section 534.
The velocity detection section 534 determines a relative velocity from the phase changes. For example, suppose that a series of obtained upbeat signals undergo phase changes by every phase θ [RXd]. Assuming that the transmission wave has an average wavelength λ, this means there is a λ/(4η/θ) change in distance every time an upbeat signal is obtained. Since this change has occurred over an interval of upbeat signal transmission Tm (=100 microseconds), the relative velocity is determined to be {λ/(4η/θ)}/Tm.
Through the above processes, a relative velocity with respect to a target as well as a distance from the target can be obtained.
[Second Variant]
The radar system 510 is able to detect a target by using a continuous wave(s) CW of one or plural frequencies. This method is especially useful in an environment where a multitude of reflected waves impinge on the radar system 510 from still objects in the surroundings, e.g., when the vehicle is in a tunnel.
The radar system 510 has an antenna array for reception purposes, including five channels of independent reception elements. In such a radar system, the azimuth-of-arrival estimation for incident reflected waves is only possible if there are four or fewer reflected waves that are simultaneously incident. In an FMCW-type radar, the number of reflected waves to be simultaneously subjected to an azimuth-of-arrival estimation can be reduced by exclusively selecting reflected waves from a specific distance. However, in an environment where a large number of still objects exist in the surroundings, e.g., in a tunnel, it is as if there were a continuum of objects to reflect radio waves; therefore, even if one narrows down on the reflected waves based on distance, the number of reflected waves may still not be equal to or smaller than four. However, any such still object in the surroundings will have an identical relative velocity with respect to the driver's vehicle, and the relative velocity will be greater than that associated with any other vehicle that is traveling ahead. On this basis, such still objects can be distinguished from any other vehicle based on the magnitudes of Doppler shifts.
Therefore, the radar system 510 performs a process of: radiating continuous waves CW of plural frequencies; and, while ignoring Doppler shift peaks that correspond to still objects in the reception signals, detecting a distance by using a Doppler shift peak(s) of any smaller shift amount(s). Unlike in the FMCW method, in the CW method, a frequency difference between a transmission wave and a reception wave is ascribable only to a Doppler shift. In other words, any peak frequency that appears in a beat signal is ascribable only to a Doppler shift.
In the description of this variant, too, a continuous wave to be used in the CW method will be referred to as a “continuous wave CW”. As described above, a continuous wave CW has a constant frequency; that is, it is unmodulated.
Suppose that the radar system 510 has radiated a continuous wave CW of a frequency fp, and detected a reflected wave of a frequency fq that has been reflected off a target. The difference between the transmission frequency fp and the reception frequency fq is called a Doppler frequency, which approximates to fp−fq=2·Vr·fp/c. Herein, Vr is a relative velocity between the radar system and the target, and c is the velocity of light. The transmission frequency fp, the Doppler frequency (fp−fq), and the velocity of light c are known. Therefore, from this equation, the relative velocity Vr=(fp−fq)·c/2fp can be determined. The distance to the target is calculated by utilizing phase information as will be described later.
In order to detect a distance to a target by using continuous waves CW, a 2 frequency CW method is adopted. In the 2 frequency CW method, continuous waves CW of two frequencies which are slightly apart are radiated each for a certain period, and their respective reflected waves are acquired. For example, in the case of using frequencies in the 76 GHz band, the difference between the two frequencies would be several hundred kHz. As will be described later, it is more preferable to determine the difference between the two frequencies while taking into account the minimum distance at which the radar used is able to detect a target.
Suppose that the radar system 510 has sequentially radiated continuous waves CW of frequencies fp1 and fp2 (fp1<fp2), and that the two continuous waves CW have been reflected off a single target, resulting in reflected waves of frequencies fq1 and fq2 being received by the radar system 510.
Based on the continuous wave CW of the frequency fp1 and the reflected wave (frequency fq1) thereof, a first Doppler frequency is obtained. Based on the continuous wave CW of the frequency fp2 and the reflected wave (frequency fq2) thereof, a second Doppler frequency is obtained. The two Doppler frequencies have substantially the same value. However, due to the difference between the frequencies fp1 and fp2, the complex signals of the respective reception waves differ in phase. By utilizing this phase information, a distance (range) to the target can be calculated.
Specifically, the radar system 510 is able to determine the distance R as R=c·Δφ/4η(fp2−fp1). Herein, Δφ denotes the phase difference between two beat signals, i.e., beat signal 1 which is obtained as a difference between the continuous wave CW of the frequency fp1 and the reflected wave (frequency fq1) thereof and beat signal 2 which is obtained as a difference between the continuous wave CW of the frequency fp2 and the reflected wave (frequency fq2) thereof. The method of identifying the frequency fb1 of beat signal 1 and the frequency fb2 of beat signal 2 is identical to that in the aforementioned instance of a beat signal from a continuous wave CW of a single frequency.
Note that a relative velocity Vr under the 2 frequency CW method is determined as follows.
Vr=fb1·c/2·fp1 or Vr=fb2·c/2·fp2
Moreover, the range in which a distance to a target can be uniquely identified is limited to the range defined by Rmax<c/2(fp2−fp1). The reason is that beat signals resulting from a reflected wave from any farther target would produce a Δφ which is greater than 2n, such that they are indistinguishable from beat signals associated with targets at closer positions. Therefore, it is more preferable to adjust the difference between the frequencies of the two continuous waves CW so that Rmax becomes greater than the minimum detectable distance of the radar. In the case of a radar whose minimum detectable distance is 100 m, fp2−fp1 may be made e.g. 1.0 MHz. In this case, Rmax=150 m, so that a signal from any target from a position beyond Rmax is not detected. In the case of mounting a radar which is capable of detection up to 250 m, fp2−fp1 may be made e.g. 500 kHz. In this case, Rmax=300 m, so that a signal from any target from a position beyond Rmax is not detected, either. In the case where the radar has both of an operation mode in which the minimum detectable distance is 100 m and the horizontal viewing angle is 120 degrees and an operation mode in which the minimum detectable distance is 250 m and the horizontal viewing angle is 5 degrees, it is preferable to switch the fp2−fp1 value be 1.0 MHz and 500 kHz for operation in the respective operation modes.
A detection approach is known which, by transmitting continuous waves CW at N different frequencies (where N is an integer of 3 or more), and utilizing phase information of the respective reflected waves, detects a distance to each target. Under this detection approach, distance can be properly recognized up to N−1 targets. As the processing to enable this, a fast Fourier transform (FFT) is used, for example. Given N=64 or 128, an FFT is performed for sampling data of a beat signal as a difference between a transmission signal and a reception signal for each frequency, thus obtaining a frequency spectrum (relative velocity). Thereafter, at the frequency of the CW wave, a further FFT is performed for peaks of the same frequency, thus to derive distance information.
Hereinafter, this will be described more specifically.
For ease of explanation, first, an instance will be described where signals of three frequencies f1, f2 and f3 are transmitted while being switched over time. It is assumed that f1>f2>f3, and f1−f2=f2−f3=Δf. A transmission time Δt is assumed for the signal wave for each frequency.
Via the transmission antenna Tx, the triangular wave/CW wave generation circuit 581 (
Each mixer 584 mixes a transmission wave and a reception wave to generate a beat signal. The A/D converter 587 converts the beat signal, which is an analog signal, into several hundred pieces of digital data (sampling data), for example.
Using the sampling data, the reception intensity calculation section 532 performs FFT computation. Through the FFT computation, frequency spectrum information of reception signals is obtained for the respective transmission frequencies f1, f2 and f3.
Thereafter, the reception intensity calculation section 532 separates peak values from the frequency spectrum information of the reception signals. The frequency of any peak value which is predetermined or greater is in proportion to a relative velocity with respect to a target. Separating a peak value(s) from the frequency spectrum information of reception signals is synonymous with separating one or plural targets with different relative velocities.
Next, with respect to each of the transmission frequencies f1 to f3, the reception intensity calculation section 532 measures spectrum information of peak values of the same relative velocity or relative velocities within a predefined range.
Now, consider a scenario where two targets A and B exist which have about the same relative velocity but are at respectively different distances. A transmission signal of the frequency f1 will be reflected from both of targets A and B to result in reception signals being obtained. The reflected waves from targets A and B will result in substantially the same beat signal frequency. Therefore, the power spectra at the Doppler frequencies of the reception signals, corresponding to their relative velocities, are obtained as a synthetic spectrum F1 into which the power spectra of two targets A and B have been merged.
Similarly, for each of the frequencies f2 and f3, the power spectra at the Doppler frequencies of the reception signals, corresponding to their relative velocities, are obtained as a synthetic spectrum F1 into which the power spectra of two targets A and B have been merged.
Under a constant difference Δf between the transmission frequencies, the phase difference between the reception signals corresponding to the respective transmission signals of the frequencies f1 and f2 is in proportion to the distance to a target. Therefore, the phase difference between the vectors f1A and f2A and the phase difference between the vectors f2A and f3A are of the same value θA, this phase difference θA being in proportion to the distance to target A. Similarly, the phase difference between the vectors f1B and f2B and the phase difference between the vectors f2B and f3B are of the same value θB, this phase difference θB being in proportion to the distance to target B.
By using a well-known method, the respective distances to targets A and B can be determined from the synthetic spectra F1 to F3 and the difference Δf between the transmission frequencies. This technique is disclosed in U.S. Pat. No. 6,703,967, for example. The entire disclosure of this publication is incorporated herein by reference.
Similar processing is also applicable when the transmitted signals have four or more frequencies.
Note that, before transmitting continuous wave CWs at N different frequencies, a process of determining the distance to and relative velocity of each target may be performed by the 2 frequency CW method. Then, under predetermined conditions, this process may be switched to a process of transmitting continuous waves CW at N different frequencies. For example, FFT computation may be performed by using the respective beat signals at the two frequencies, and if the power spectrum of each transmission frequency undergoes a change over time of 30% or more, the process may be switched. The amplitude of a reflected wave from each target undergoes a large change over time due to multipath influences and the like. When there exists a change of a predetermined magnitude or greater, it may be considered that plural targets may exist.
Moreover, the CW method is known to be unable to detect a target when the relative velocity between the radar system and the target is zero, i.e., when the Doppler frequency is zero. However, when a pseudo Doppler signal is determined by the following methods, for example, it is possible to detect a target by using that frequency.
(Method 1) A mixer that causes a certain frequency shift in the output of a receiving antenna is added. By using a transmission signal and a reception signal with a shifted frequency, a pseudo Doppler signal can be obtained.
(Method 2) A variable phase shifter to introduce phase changes continuously over time is inserted between the output of a receiving antenna and a mixer, thus adding a pseudo phase difference to the reception signal. By using a transmission signal and a reception signal with an added phase difference, a pseudo Doppler signal can be obtained.
An example of specific construction and operation of inserting a variable phase shifter to generate a pseudo Doppler signal under Method 2 is disclosed in Japanese Laid-Open Patent Publication No. 2004-257848. The entire disclosure of this publication is incorporated herein by reference.
When targets with zero or very little relative velocity need to be detected, the aforementioned processes of generating a pseudo Doppler signal may be adopted, or the process may be switched to a target detection process under the FMCW method.
Next, with reference to
The example below will illustrate a case where continuous waves CW are transmitted at two different frequencies fp1 and fp2 (fp1<fp2), and the phase information of each reflected wave is utilized to respectively detect a distance with respect to a target.
At step S41, the triangular wave/CW wave generation circuit 581 generates two continuous waves CW of frequencies which are slightly apart, i.e., frequencies fp1 and fp2.
At step S42, the transmission antenna Tx and the reception antennas Rx perform transmission/reception of the generated series of continuous waves CW. Note that the process of step S41 and the process of step S42 are to be performed in parallel fashion respectively by the triangular wave/CW wave generation circuit 581 and the transmission antenna element Tx/reception antenna Rx, rather than step S42 following only after completion of step S41.
At step S43, each mixer 584 generates a difference signal by utilizing each transmission wave and each reception wave, whereby two difference signals are obtained. Each reception wave is inclusive of a reception wave emanating from a still object and a reception wave emanating from a target. Therefore, next, a process of identifying frequencies to be utilized as the beat signals is performed. Note that the process of step S41, the process of step S42, and the process of step S43 are to be performed in parallel fashion by the triangular wave/CW wave generation circuit 581, the transmission antenna Tx/reception antenna Rx, and the mixers 584, rather than step S42 following only after completion of step S41, or step S43 following only after completion of step S42.
At step S44, for each of the two difference signals, the object detection apparatus 570 identifies certain peak frequencies to be frequencies fb1 and fb2 of beat signals, such that these frequencies are equal to or smaller than a frequency which is predefined as a threshold value and yet they have amplitude values which are equal to or greater than a predetermined amplitude value, and that the difference between the two frequencies is equal to or smaller than a predetermined value.
At step S45, based on one of the two beat signal frequencies identified, the reception intensity calculation section 532 detects a relative velocity. The reception intensity calculation section 532 calculates the relative velocity according to Vr=fb1·c/2·fp1, for example. Note that a relative velocity may be calculated by utilizing each of the two beat signal frequencies, which will allow the reception intensity calculation section 532 to verify whether they match or not, thus enhancing the precision of relative velocity calculation.
At step S46, the reception intensity calculation section 532 determines a phase difference Δφ between two beat signals 1 and 2, and determines a distance R=c·Δφ/4η(fp2−fp1) to the target.
Through the above processes, the relative velocity and distance to a target can be detected.
Note that continuous waves CW may be transmitted at N different frequencies (where N is 3 or more), and by utilizing phase information of the respective reflected wave, distances to plural targets which are of the same relative velocity but at different positions may be detected.
In addition to the radar system 510, the vehicle 500 described above may further include another radar system. For example, the vehicle 500 may further include a radar system having a detection range toward the rear or the sides of the vehicle body. In the case of incorporating a radar system having a detection range toward the rear of the vehicle body, the radar system may monitor the rear, and if there is any danger of having another vehicle bump into the rear, make a response by issuing an alarm, for example. In the case of incorporating a radar system having a detection range toward the sides of the vehicle body, the radar system may monitor an adjacent lane when the driver's vehicle changes its lane, etc., and make a response by issuing an alarm or the like as necessary.
The applications of the above-described radar system 510 are not limited to onboard use only. Rather, the radar system 510 may be used as sensors for various purposes. For example, it may be used as a radar for monitoring the surroundings of a house or any other building.
Alternatively, it may be used as a sensor for detecting the presence or absence of a person at a specific indoor place, or whether or not such a person is undergoing any motion, etc., without utilizing any optical images.
[Supplementary Details of Processing]
Other embodiments will be described in connection with the 2 frequency CW or FMCW techniques for array antennas as described above. As described earlier, in the example of
In order to solve this problem, a scalar signal may be generated as a beat signal. For each of a plurality of beat signals that have been generated, two complex Fourier transforms may be performed with respect to the spatial axis direction, which conforms to the antenna array, and to the time axis direction, which conforms to the lapse of time, thus to obtain results of frequency analysis. As a result, with only a small amount of computation, beam formation can eventually be achieved so that directions of arrival of reflected waves can be identified, whereby results of frequency analysis can be obtained for the respective beams. As a patent document related to the present disclosure, the entire disclosure of the specification of U.S. Pat. No. 6,339,395 is incorporated herein by reference.
[Optical Sensor, e.g., Camera, and Millimeter Wave Radar]
Next, a comparison between the above-described array antenna and conventional antennas, as well as an exemplary application in which both of the present array antenna and an optical sensor (e.g., a camera) are utilized, will be described. Note that LIDAR or the like may be employed as the optical sensor.
A millimeter wave radar is able to directly detect a distance (range) to a target and a relative velocity thereof. Another characteristic is that its detection performance is not much deteriorated in the nighttime (including dusk), or in bad weather, e.g., rainfall, fog, or snowfall. On the other hand, it is believed that it is not just as easy for a millimeter wave radar to take a two-dimensional grasp of a target as it is for a camera. On the other hand, it is relatively easy for a camera to take a two-dimensional grasp of a target and recognize its shape. However, a camera may not be able to image a target in nighttime or bad weather, which presents a considerable problem. This problem is particularly outstanding when droplets of water have adhered to the portion through which to ensure lighting, or the eyesight is narrowed by a fog. This problem similarly exists for LIDAR or the like, which also pertains to the realm of optical sensors.
In these years, in answer to increasing demand for safer vehicle operation, driver assist systems for preventing collisions or the like are being developed. A driver assist system acquires an image in the direction of vehicle travel with a sensor such as a camera or a millimeter wave radar, and when any obstacle is recognized that is predicted to hinder vehicle travel, brakes or the like are automatically applied to prevent collisions or the like. Such a function of collision avoidance is expected to operate normally, even in nighttime or bad weather.
Hence, driver assist systems of a so-called fusion construction are gaining prevalence, where, in addition to a conventional optical sensor such as a camera, a millimeter wave radar is mounted as a sensor, thus realizing a recognition process that takes advantage of both. Such a driver assist system will be discussed later.
On the other hand, higher and higher functions are being required of the millimeter wave radar itself. A millimeter wave radar for onboard use mainly uses electromagnetic waves of the 76 GHz band. The antenna power of its antenna is restricted to below a certain level under each country's law or the like. For example, it is restricted to 0.01 W or below in Japan. Under such restrictions, a millimeter wave radar for onboard use is expected to satisfy the required performance that, for example, its detection range is 200 m or more; the antenna size is 60 mm×60 mm or less; its horizontal detection angle is 90 degrees or more; its range resolution is 20 cm or less; it is capable of short-range detection within 10 m; and so on. Conventional millimeter wave radars have used microstrip lines as waveguides, and patch antennas as antennas (hereinafter, these will both be referred to as “patch antennas”). However, with a patch antenna, it has been difficult to attain the aforementioned performance.
By using a slot array antenna to which the technique of the present disclosure is applied, the inventors have successfully achieved the aforementioned performance. As a result, a millimeter wave radar has been realized which is smaller in size, more efficient, and higher-performance than are conventional patch antennas and the like. In addition, by combining this millimeter wave radar and an optical sensor such as a camera, a small-sized, highly efficient, and high-performance fusion apparatus has been realized which has existed never before. This will be described in detail below.
[Installment of Millimeter Wave Radar within Vehicle Room]
A conventional patch antenna-based millimeter wave radar 510′ is placed behind and inward of a grill 512 which is at the front nose of a vehicle. An electromagnetic wave that is radiated from an antenna goes through the apertures in the grill 512, and is radiated ahead of the vehicle 500. In this case, no dielectric layer, e.g., glass, exists that decays or reflects electromagnetic wave energy, in the region through which the electromagnetic wave passes. As a result, an electromagnetic wave that is radiated from the patch antenna-based millimeter wave radar 510′ reaches over a long range, e.g., to a target which is 150 m or farther away. By receiving with the antenna the electromagnetic wave reflected therefrom, the millimeter wave radar 510′ is able to detect a target. In this case, however, since the antenna is placed behind and inward of the grill 512 of the vehicle, the radar may be broken when the vehicle collides into an obstacle. Moreover, it may be soiled with mud or the like in rain, etc., and the soil that has adhered to the antenna may hinder radiation and reception of electromagnetic waves.
Similarly to the conventional manner, the millimeter wave radar 510 incorporating a slot array antenna according to an embodiment of the present disclosure may be placed behind the grill 512, which is located at the front nose of the vehicle (not shown). This allows the energy of the electromagnetic wave to be radiated from the antenna to be utilized by 100%, thus enabling long-range detection beyond the conventional level, e.g., detection of a target which is at a distance of 250 m or more.
Furthermore, the millimeter wave radar 510 according to an embodiment of the present disclosure can also be placed within the vehicle room, i.e., inside the vehicle. In that case, the millimeter wave radar 510 is placed inward of the windshield 511 of the vehicle, to fit in a space between the windshield 511 and a face of the rearview mirror (not shown) that is opposite to its specular surface. On the other hand, the conventional patch antenna-based millimeter wave radar 510′ cannot be placed inside the vehicle room mainly for the two following reasons. A first reason is its large size, which prevents itself from being accommodated within the space between the windshield 511 and the rearview mirror. A second reason is that an electromagnetic wave that is radiated ahead reflects off the windshield 511 and decays due to dielectric loss, thus becoming unable to travel the desired distance. As a result, if a conventional patch antenna-based millimeter wave radar is placed within the vehicle room, only targets which are 100 m ahead or less can be detected, for example. On the other hand, a millimeter wave radar according to an embodiment of the present disclosure is able to detect a target which is at a distance of 200 m or more, despite reflection or decay at the windshield 511. This performance is equivalent to, or even greater than, the case where a conventional patch antenna-based millimeter wave radar is placed outside the vehicle room.
[Fusion Construction Based on Millimeter Wave Radar and Camera, Etc., being Placed within Vehicle Room]
Currently, an optical imaging device such as a CCD camera is used as the main sensor in many a driver assist system (Driver Assist System). Usually, a camera or the like is placed within the vehicle room, inward of the windshield 511, in order to account for unfavorable influences of the external environment, etc. In this context, in order to minimize the optical effect of raindrops and the like, the camera or the like is placed in a region which is swept by the wipers (not shown) but is inward of the windshield 511.
In recent years, due to needs for improved performance of a vehicle in terms of e.g. automatic braking, there has been a desire for automatic braking or the like that is guaranteed to work regardless of whatever external environment may exist. In this case, if the only sensor in the driver assist system is an optical device such as a camera, a problem exists in that reliable operation is not guaranteed in nighttime or bad weather. This has led to the need for a driver assist system that incorporates not only an optical sensor (such as a camera) but also a millimeter wave radar, these being used for cooperative processing, so that reliable operation is achieved even in nighttime or bad weather.
As described earlier, a millimeter wave radar incorporating the present slot array antenna permits itself to be placed within the vehicle room, due to downsizing and remarkable enhancement in the efficiency of the radiated electromagnetic wave over that of a conventional patch antenna. By taking advantage of these properties, as shown in
(1) It is easier to install the driver assist system on the vehicle 500. The conventional patch antenna-based millimeter wave radar 510′ has required a space behind the grill 512, which is at the front nose, in order to accommodate the radar. Since this space may include some sites that affect the structural design of the vehicle, if the size of the radar device is changed, it may have been necessary to reconsider the structural design. This inconvenience is avoided by placing the millimeter wave radar within the vehicle room.
(2) Free from the influences of rain, nighttime, or other external environment factors to the vehicle, more reliable operation can be achieved. Especially, as shown in
(3) Reliability of the millimeter wave radar device is improved. As described above, since the conventional patch antenna-based millimeter wave radar 510′ is placed behind the grill 512, which is at the front nose, it is likely to gather soil, and may be broken even in a minor collision accident or the like. For these reasons, cleaning and functionality checks are always needed. Moreover, as will be described below, if the position or direction of attachment of the millimeter wave radar becomes shifted due to an accident or the like, it is necessary to reestablish alignment with respect to the camera. The chances of such occurrences are reduced by placing the millimeter wave radar within the vehicle room, whereby the aforementioned inconveniences are avoided.
In a driver assist system of such fusion construction, the optical sensor, e.g., a camera, and the millimeter wave radar 510 incorporating the present slot array antenna may have an integrated construction, i.e., being in fixed position with respect to each other. In that case, certain relative positioning should be kept between the optical axis of the optical sensor such as a camera and the directivity of the antenna of the millimeter wave radar, as will be described later. When this driver assist system having an integrated construction is fixed within the vehicle room of the vehicle 500, the optical axis of the camera, etc., should be adjusted so as to be oriented in a certain direction ahead of the vehicle. For these matters, see the specification of US Patent Application Publication No. 2015/0264230, the specification of US Patent Application Publication No. 2016/0264065, U.S. patent application Ser. No. 15/248,141, U.S. patent application Ser. No. 15/248,149, and U.S. patent application Ser. No. 15/248,156, which are incorporated herein by reference. Related techniques concerning the camera are described in the specification of U.S. Pat. No. 7,355,524, and the specification of U.S. Pat. No. 7,420,159, the entire disclosure of each which is incorporated herein by reference.
Regarding placement of an optical sensor such as a camera and a millimeter wave radar within the vehicle room, see, for example, the specification of U.S. Pat. No. 8,604,968, the specification of U.S. Pat. No. 8,614,640, and the specification of U.S. Pat. No. 7,978,122, the entire disclosure of each which is incorporated herein by reference. However, at the time when these patents were filed for, only conventional antennas with patch antennas were the known millimeter wave radars, and thus observation was not possible over sufficient distances. For example, the distance that is observable with a conventional millimeter wave radar is considered to be at most 100 m to 150 m. Moreover, when a millimeter wave radar is placed inward of the windshield, the large radar size inconveniently blocks the driver's field of view, thus hindering safe driving. On the other hand, a millimeter wave radar incorporating a slot array antenna according to an embodiment of the present disclosure is capable of being placed within the vehicle room because of its small size and remarkable enhancement in the efficiency of the radiated electromagnetic wave over that of a conventional patch antenna. This enables a long-range observation over 200 m, while not blocking the driver's field of view.
[Adjustment of Position of Attachment Between Millimeter Wave Radar and Camera, Etc.,]
In the processing under fusion construction (which hereinafter may be referred to as a “fusion process”), it is desired that an image which is obtained with a camera or the like and the radar information which is obtained with the millimeter wave radar map onto the same coordinate system because, if they differ as to position and target size, cooperative processing between both will be hindered.
This involves adjustment from the following three standpoints.
(1) The optical axis of the camera or the like and the antenna directivity of the millimeter wave radar must have a certain fixed relationship.
It is required that the optical axis of the camera or the like and the antenna directivity of the millimeter wave radar are matched. Alternatively, a millimeter wave radar may include two or more transmission antennas and two or more reception antennas, the directivities of these antennas being intentionally made different. Therefore, it is necessary to guarantee that at least a certain known relationship exists between the optical axis of the camera or the like and the directivities of these antennas.
In the case where the camera or the like and the millimeter wave radar have the aforementioned integrated construction, i.e., being in fixed position to each other, the relative positioning between the camera or the like and the millimeter wave radar stays fixed. Therefore, the aforementioned requirements are satisfied with respect to such an integrated construction. On the other hand, in a conventional patch antenna or the like, where the millimeter wave radar is placed behind the grill 512 of the vehicle 500, the relative positioning between them is usually to be adjusted according to (2) below.
(2) A certain fixed relationship exists between an image acquired with the camera or the like and radar information of the millimeter wave radar in an initial state (e.g., upon shipment) of having been attached to the vehicle.
The positions of attachment of the optical sensor such as a camera and the millimeter wave radar 510 or 510′ on the vehicle 500 will finally be determined in the following manner. At a predetermined position 800 ahead of the vehicle 500, a chart to serve as a reference or a target which is subject to observation by the radar (which will hereinafter be referred to as, respectively, a “reference chart” and a “reference target”, and collectively as the “benchmark”) is accurately positioned. This is observed with an optical sensor such as a camera or with the millimeter wave radar 510. The observation information regarding the observed benchmark is compared against previously-stored shape information or the like of the benchmark, and the current offset information is quantitated. Based on this offset information, by at least one of the following means, the positions of attachment of an optical sensor such as a camera and the millimeter wave radar 510 or 510′ are adjusted or corrected. Any other means may also be employed that can provide similar results.
(i) Adjust the positions of attachment of the camera and the millimeter wave radar so that the benchmark will come at a midpoint between the camera and the millimeter wave radar. This adjustment may be done by using a jig or tool, etc., which is separately provided.
(ii) Determine an offset amounts of the camera and the axis/directivity of the millimeter wave radar relative to the benchmark, and through image processing of the camera image and radar processing, correct for these offset amounts in the axis/directivity.
What is to be noted is that, in the case where the optical sensor such as a camera and the millimeter wave radar 510 incorporating a slot array antenna according to an embodiment of the present disclosure have an integrated construction, i.e., being in fixed position to each other, adjusting an offset of either the camera or the radar with respect to the benchmark will make the offset amount known for the other as well, thus making it unnecessary to check for the other's offset with respect to the benchmark.
Specifically, with respect to the onboard camera system 700, a reference chart may be placed at a predetermined position 750, and an image taken by the camera is compared against advance information indicating where in the field of view of the camera the reference chart image is supposed to be located, thereby detecting an offset amount. Based on this, the camera is adjusted by at least one of the above means (i) and (ii). Next, the offset amount which has been ascertained for the camera is translated into an offset amount of the millimeter wave radar. Thereafter, an offset amount adjustment is made with respect to the radar information, by at least one of the above means (i) and (ii).
Alternatively, this may be performed on the basis of the millimeter wave radar 510. In other words, with respect to the millimeter wave radar 510, a reference target may be placed at a predetermined position 800, and the radar information thereof is compared against advance information indicating where in the field of view of the millimeter wave radar 510 the reference target is supposed to be located, thereby detecting an offset amount. Based on this, the millimeter wave radar 510 is adjusted by at least one of the above means (i) and (ii). Next, the offset amount which has been ascertained for the millimeter wave radar is translated into an offset amount of the camera. Thereafter, an offset amount adjustment is made with respect to the image information obtained by the camera, by at least one of the above means (i) and (ii).
(3) Even after an initial state of the vehicle, a certain relationship is maintained between an image acquired with the camera or the like and radar information of the millimeter wave radar.
Usually, an image acquired with the camera or the like and radar information of the millimeter wave radar are supposed to be fixed in the initial state, and hardly vary unless in an accident of the vehicle or the like. However, if an offset in fact occurs between these, an adjustment is possible by the following means.
The camera is attached in such a manner that portions 513 and 514 (characteristic points) that are characteristic of the driver's vehicle fit within its field of view, for example. The positions at which these characteristic points are actually imaged by the camera are compared against the information of the positions to be assumed by these characteristic points when the camera is attached accurately in place, and an offset amount(s) is detected therebetween. Based on this detected offset amount(s), the position of any image that is taken thereafter may be corrected, whereby an offset of the physical position of attachment of the camera can be corrected for. If this correction sufficiently embodies the performance that is required of the vehicle, then the adjustment per the above (2) may not be needed. By regularly performing this adjustment during startup or operation of the vehicle 500, even if an offset of the camera or the like occurs anew, it is possible to correct for the offset amount, thus helping safe travel.
However, this means is generally considered to result in poorer accuracy of adjustment than with the above means (2). When making an adjustment based on an image which is obtained by imaging a benchmark with the camera, the azimuth of the benchmark can be determined with a high precision, whereby a high accuracy of adjustment can be easily achieved. However, since this means utilizes a part of the vehicle body for the adjustment instead of a benchmark, it is rather difficult to enhance the accuracy of azimuth determination. Thus, the resultant accuracy of adjustment will be somewhat inferior. However, it may still be effective as a means of correction when the position of attachment of the camera or the like is considerably altered for reasons such as an accident or a large external force being applied to the camera or the like within the vehicle room, etc.
[Mapping of Target as Detected by Millimeter Wave Radar and Camera or the Like: Matching Process]
In a fusion process, for a given target, it needs to be established that an image thereof which is acquired with a camera or the like and radar information which is acquired with the millimeter wave radar pertain to “the same target”. For example, suppose that two obstacles (first and second obstacles), e.g., two bicycles, have appeared ahead of the vehicle 500. These two obstacles will be captured as camera images, and detected as radar information of the millimeter wave radar. At this time, the camera image and the radar information with respect to the first obstacle need to be mapped to each other so that they are both directed to the same target. Similarly, the camera image and the radar information with respect to the second obstacle need to be mapped to each other so that they are both directed to the same target. If the camera image of the first obstacle and the radar information of the second obstacle are mistakenly recognized to pertain to an identical object, a considerable accident may occur. Hereinafter, in the present specification, such a process of determining whether a target in the camera image and a target in the radar image pertain to the same target may be referred to as a “matching process”.
This matching process may be implemented by various detection devices (or methods) described below. Hereinafter, these will be specifically described. Note that the each of the following detection devices is to be installed in the vehicle, and at least includes a millimeter wave radar detection section, an image detection section (e.g., a camera) which is oriented in a direction overlapping the direction of detection by the millimeter wave radar detection section, and a matching section. Herein, the millimeter wave radar detection section includes a slot array antenna according to any of the embodiments of the present disclosure, and at least acquires radar information in its own field of view. The image acquisition section at least acquires image information in its own field of view. The matching section includes a processing circuit which matches a result of detection by the millimeter wave radar detection section against a result of detection by the image detection section to determine whether or not the same target is being detected by the two detection sections. Herein, the image detection section may be composed of a selected one of, or selected two or more of, an optical camera, LIDAR, an infrared radar, and an ultrasonic radar. The following detection devices differ from one another in terms of the detection process at their respective matching section.
In a first detection device, the matching section performs two matches as follows. A first match involves, for a target of interest that has been detected by the millimeter wave radar detection section, obtaining distance information and lateral position information thereof, and also finding a target that is the closest to the target of interest among a target or two or more targets detected by the image detection section, and detecting a combination(s) thereof. A second match involves, for a target of interest that has been detected by the image detection section, obtaining distance information and lateral position information thereof, and also finding a target that is the closest to the target of interest among a target or two or more targets detected by the millimeter wave radar detection section, and detecting a combination(s) thereof. Furthermore, this matching section determines whether there is any matching combination between the combination(s) of such targets as detected by the millimeter wave radar detection section and the combination(s) of such targets as detected by the image detection section. Then, if there is any matching combination, it is determined that the same object is being detected by the two detection sections. In this manner, a match is attained between the respective targets that have been detected by the millimeter wave radar detection section and the image detection section.
A related technique is described in the specification of U.S. Pat. No. 7,358,889, the entire disclosure of which is incorporated herein by reference. In this publication, the image detection section is illustrated by way of a so-called stereo camera that includes two cameras. However, this technique is not limited thereto. In the case where the image detection section includes a single camera, detected targets may be subjected to an image recognition process or the like as appropriate, in order to obtain distance information and lateral position information of the targets. Similarly, a laser sensor such as a laser scanner may be used as the image detection section.
In a second detection device, the matching section matches a result of detection by the millimeter wave radar detection section and a result of detection by the image detection section every predetermined period of time. If the matching section determines that the same target was being detected by the two detection sections in the previous result of matching, it performs a match by using this previous result of matching. Specifically, the matching section matches a target which is currently detected by the millimeter wave radar detection section and a target which is currently detected by the image detection section, against the target which was determined in the previous result of matching to be being detected by the two detection sections. Then, based on the result of matching for the target which is currently detected by the millimeter wave radar detection section and the result of matching for the target which is currently detected by the image detection section, the matching section determines whether or not the same target is being detected by the two detection sections. Thus, rather than directly matching the results of detection by the two detection sections, this detection device performs a chronological match between the two results of detection and a previous result of matching. Therefore, the accuracy of detection is improved over the case of only performing a momentary match, whereby stable matching is realized. In particular, even if the accuracy of the detection section drops momentarily, matching is still possible because of utilizing past results of matching. Moreover, by utilizing the previous result of matching, this detection device is able to easily perform a match between the two detection sections.
In the current match which utilizes the previous result of matching, if the matching section of this detection device determines that the same object is being detected by the two detection sections, then the matching section of this detection device excludes this determined object in performing matching between objects which are currently detected by the millimeter wave radar detection section and objects which are currently detected by the image detection section. Then, this matching section determines whether there exists any identical object that is currently detected by the two detection sections. Thus, while taking into account the result of chronological matching, the detection device also makes a momentary match based on two results of detection that are obtained from moment to moment. As a result, the detection device is able to surely perform a match for any object that is detected during the current detection.
A related technique is described in the specification of U.S. Pat. No. 7,417,580, the entire disclosure of which is incorporated herein by reference. In this publication, the image detection section is illustrated by way of a so-called stereo camera that includes two cameras. However, this technique is not limited thereto. In the case where the image detection section includes a single camera, detected targets may be subjected to an image recognition process or the like as appropriate, in order to obtain distance information and lateral position information of the targets. Similarly, a laser sensor such as a laser scanner may be used as the image detection section.
In a third detection device, the two detection sections and matching section perform detection of targets and performs matches therebetween at predetermined time intervals, and the results of such detection and the results of such matching are chronologically stored to a storage medium, e.g., memory. Then, based on a rate of change in the size of a target in the image as detected by the image detection section, and on a distance to a target from the driver's vehicle and its rate of change (relative velocity with respect to the driver's vehicle) as detected by the millimeter wave radar detection section, the matching section determines whether the target which has been detected by the image detection section and the target which has been detected by the millimeter wave radar detection section are an identical object.
When determining that these targets are an identical object, based on the position of the target in the image as detected by the image detection section, and on the distance to the target from the driver's vehicle and/or its rate of change as detected by the millimeter wave radar detection section, the matching section predicts a possibility of collision with the vehicle.
A related technique is described in the specification of U.S. Pat. No. 6,903,677, the entire disclosure of which is incorporated herein by reference.
As described above, in a fusion process of a millimeter wave radar and an imaging device such as a camera, an image which is obtained with the camera or the like and radar information which is obtained with the millimeter wave radar are matched against each other. A millimeter wave radar incorporating the aforementioned array antenna according to an embodiment of the present disclosure can be constructed so as to have a small size and high performance. Therefore, high performance and downsizing, etc., can be achieved for the entire fusion process including the aforementioned matching process. This improves the accuracy of target recognition, and enables safer travel control for the vehicle.
[Other Fusion Processes]
In a fusion process, various functions are realized based on a matching process between an image which is obtained with a camera or the like and radar information which is obtained with the millimeter wave radar detection section. Examples of processing apparatuses that realize representative functions of a fusion process will be described below.
Each of the following processing apparatuses is to be installed in a vehicle, and at least includes: a millimeter wave radar detection section to transmit or receive electromagnetic waves in a predetermined direction; an image acquisition section, such as a monocular camera, that has a field of view overlapping the field of view of the millimeter wave radar detection section; and a processing section which obtains information therefrom to perform target detection and the like. The millimeter wave radar detection section acquires radar information in its own field of view. The image acquisition section acquires image information in its own field of view. A selected one, or selected two or more of, an optical camera, LIDAR, an infrared radar, and an ultrasonic radar may be used as the image acquisition section. The processing section can be implemented by a processing circuit which is connected to the millimeter wave radar detection section and the image acquisition section. The following processing apparatuses differ from one another with respect to the content of processing by this processing section.
In a first processing apparatus, the processing section extracts, from an image which is captured by the image acquisition section, a target which is recognized to be the same as the target which is detected by the millimeter wave radar detection section. In other words, a matching process according to the aforementioned detection device is performed. Then, it acquires information of a right edge and a left edge of the extracted target image, and derives locus approximation lines, which are straight lines or predetermined curved lines for approximating loci of the acquired right edge and the left edge, are derived for both edges. The edge which has a larger number of edges existing on the locus approximation line is selected as a true edge of the target. The lateral position of the target is derived on the basis of the position of the edge that has been selected as a true edge. This permits a further improvement on the accuracy of detection of a lateral position of the target.
A related technique is described in the specification of U.S. Pat. No. 8,610,620, the entire disclosure of which is incorporated herein by reference.
In a second processing apparatus, in determining the presence of a target, the processing section alters a determination threshold to be used in checking for a target presence in radar information, on the basis of image information. Thus, if a target image that may be an obstacle to vehicle travel has been confirmed with a camera or the like, or if the presence of a target has been estimated, etc., for example, the determination threshold for the target detection by the millimeter wave radar detection section can be optimized so that more accurate target information can be obtained. In other words, if the possibility of the presence of an obstacle is high, the determination threshold is altered so that this processing apparatus will surely be activated. On the other hand, if the possibility of the presence of an obstacle is low, the determination threshold is altered so that unwanted activation of this processing apparatus is prevented. This permits appropriate activation of the system.
Furthermore in this case, based on radar information, the processing section may designate a region of detection for the image information, and estimate a possibility of the presence of an obstacle on the basis of image information within this region. This makes for a more efficient detection process.
A related technique is described in the specification of U.S. Pat. No. 7,570,198, the entire disclosure of which is incorporated herein by reference.
In a third processing apparatus, the processing section performs combined displaying where images obtained from a plurality of different imaging devices and a millimeter wave radar detection section and an image signal based on radar information are displayed on at least one display device. In this displaying process, horizontal and vertical synchronizing signals are synchronized between the plurality of imaging devices and the millimeter wave radar detection section, and among the image signals from these devices, selective switching to a desired image signal is possible within one horizontal scanning period or one vertical scanning period. This allows, on the basis of the horizontal and vertical synchronizing signals, images of a plurality of selected image signals to be displayed side by side; and, from the display device, a control signal for setting a control operation in the desired imaging device and the millimeter wave radar detection section is sent.
When a plurality of different display devices display respective images or the like, it is difficult to compare the respective images against one another. Moreover, when display devices are provided separately from the third processing apparatus itself, there is poor operability for the device. The third processing apparatus would overcome such shortcomings.
A related technique is described in the specification of U.S. Pat. No. 6,628,299 and the specification of U.S. Pat. No. 7,161,561, the entire disclosure of each of which is incorporated herein by reference.
In a fourth processing apparatus, with respect to a target which is ahead of a vehicle, the processing section instructs an image acquisition section and a millimeter wave radar detection section to acquire an image and radar information containing that target. From within such image information, the processing section determines a region in which the target is contained. Furthermore, the processing section extracts radar information within this region, and detects a distance from the vehicle to the target and a relative velocity between the vehicle and the target. Based on such information, the processing section determines a possibility that the target will collide against the vehicle. This enables an early detection of a possible collision with a target.
A related technique is described in the specification of U.S. Pat. No. 8,068,134, the entire disclosure of which is incorporated herein by reference.
In a fifth processing apparatus, based on radar information or through a fusion process which is based on radar information and image information, the processing section recognizes a target or two or more targets ahead of the vehicle. The “target” encompasses any moving entity such as other vehicles or pedestrians, traveling lanes indicated by white lines on the road, road shoulders and any still objects (including gutters, obstacles, etc.), traffic lights, pedestrian crossings, and the like that may be there. The processing section may encompass a GPS (Global Positioning System) antenna. By using a GPS antenna, the position of the driver's vehicle may be detected, and based on this position, a storage device (referred to as a map information database device) that stores road map information may be searched in order to ascertain a current position on the map. This current position on the map may be compared against a target or two or more targets that have been recognized based on radar information or the like, whereby the traveling environment may be recognized. On this basis, the processing section may extract any target that is estimated to hinder vehicle travel, find safer traveling information, and display it on a display device, as necessary, to inform the driver.
A related technique is described in the specification of U.S. Pat. No. 6,191,704, the entire disclosure of which is incorporated herein by reference.
The fifth processing apparatus may further include a data communication device (having communication circuitry) that communicates with a map information database device which is external to the vehicle. The data communication device may access the map information database device, with a period of e.g. once a week or once a month, to download the latest map information therefrom. This allows the aforementioned processing to be performed with the latest map information.
Furthermore, the fifth processing apparatus may compare between the latest map information that was acquired during the aforementioned vehicle travel and information that is recognized of a target or two or more targets based on radar information, etc., in order to extract target information (hereinafter referred to as “map update information”) that is not included in the map information. Then, this map update information may be transmitted to the map information database device via the data communication device. The map information database device may store this map update information in association with the map information that is within the database, and update the current map information itself, if necessary. In performing the update, respective pieces of map update information that are obtained from a plurality of vehicles may be compared against one another to check certainty of the update.
Note that this map update information may contain more detailed information than the map information which is carried by any currently available map information database device. For example, schematic shapes of roads may be known from commonly-available map information, but it typically does not contain information such as the width of the road shoulder, the width of the gutter that may be there, any newly occurring bumps or dents, shapes of buildings, and so on. Neither does it contain heights of the roadway and the sidewalk, how a slope may connect to the sidewalk, etc. Based on conditions which are separately set, the map information database device may store such detailed information (hereinafter referred to as “map update details information”) in association with the map information. Such map update details information provides a vehicle (including the driver's vehicle) with information which is more detailed than the original map information, thereby rending itself available for not only the purpose of ensuring safe vehicle travel but also some other purposes. As used herein, a “vehicle (including the driver's vehicle)” may be e.g. an automobile, a motorcycle, a bicycle, or any autonomous vehicle to become available in the future, e.g., an electric wheelchair. The map update details information is to be used when any such vehicle may travel.
(Recognition Via Neural Network)
Each of the first to fifth processing apparatuses may further include a sophisticated apparatus of recognition. The sophisticated apparatus of recognition may be provided external to the vehicle. In that case, the vehicle may include a high-speed data communication device that communicates with the sophisticated apparatus of recognition. The sophisticated apparatus of recognition may be constructed from a neural network, which may encompass so-called deep learning and the like. This neural network may include a convolutional neural network (hereinafter referred to as “CNN”), for example. A CNN, a neural network that has proven successful in image recognition, is characterized by possessing one or more sets of two layers, namely, a convolutional layer and a pooling layer.
There exists at least three kinds of information as follows, any of which may be input to a convolutional layer in the processing apparatus:
(1) information that is based on radar information which is acquired by the millimeter wave radar detection section;
(2) information that is based on specific image information which is acquired, based on radar information, by the image acquisition section; or
(3) fusion information that is based on radar information and image information which is acquired by the image acquisition section, or information that is obtained based on such fusion information.
Based on information of any of the above kinds, or information based on a combination thereof, product-sum operations corresponding to a convolutional layer are performed. The results are input to the subsequent pooling layer, where data is selected according to a predetermined rule. In the case of max pooling where a maximum value among pixel values is chosen, for example, the rule may dictate that a maximum value be chosen for each split region in the convolutional layer, this maximum value being regarded as the value of the corresponding position in the pooling layer.
A sophisticated apparatus of recognition that is composed of a CNN may include a single set of a convolutional layer and a pooling layer, or a plurality of such sets which are cascaded in series. This enables accurate recognition of a target, which is contained in the radar information and the image information, that may be around a vehicle.
Related techniques are described in the U.S. Pat. No. 8,861,842, the specification of U.S. Pat. No. 9,286,524, and the specification of US Patent Application Publication No. 2016/0140424, the entire disclosure of each of which is incorporated herein by reference.
In a sixth processing apparatus, the processing section performs processing that is related to headlamp control of a vehicle. When a vehicle travels in nighttime, the driver may check whether another vehicle or a pedestrian exists ahead of the driver's vehicle, and control a beam(s) from the headlamp(s) of the driver's vehicle to prevent the driver of the other vehicle or the pedestrian from being dazzled by the headlamp(s) of the driver's vehicle. This sixth processing apparatus automatically controls the headlamp(s) of the driver's vehicle by using radar information, or a combination of radar information and an image taken by a camera or the like.
Based on radar information, or through a fusion process based on radar information and image information, the processing section detects a target that corresponds to a vehicle or pedestrian ahead of the vehicle. In this case, a vehicle ahead of a vehicle may encompass a preceding vehicle that is ahead, a vehicle or a motorcycle in the oncoming lane, and so on. When detecting any such target, the processing section issues a command to lower the beam(s) of the headlamp(s). Upon receiving this command, the control section (control circuit) which is internal to the vehicle may control the headlamp(s) to lower the beam(s) therefrom.
Related techniques are described in the specification of U.S. Pat. No. 6,403,942, the specification of U.S. Pat. No. 6,611,610, the specification of U.S. Pat. No. 8,543,277, the specification of U.S. Pat. No. 8,593,521, and the specification of U.S. Pat. No. 8,636,393, the entire disclosure of each of which is incorporated herein by reference.
According to the above-described processing by the millimeter wave radar detection section, and the above-described fusion process by the millimeter wave radar detection section and an imaging device such as a camera, the millimeter wave radar can be constructed so as to have a small size and high performance, whereby high performance and downsizing, etc., can be achieved for the radar processing or the entire fusion process. This improves the accuracy of target recognition, and enables safer travel control for the vehicle.
<Application Example 2: Various Monitoring Systems (Natural Elements, Buildings, Roads, Watch, Security)>
A millimeter wave radar (radar system) incorporating an array antenna according to an embodiment of the present disclosure also has a wide range of applications in the fields of monitoring, which may encompass natural elements, weather, buildings, security, nursing care, and the like. In a monitoring system in this context, a monitoring apparatus that includes the millimeter wave radar may be installed e.g. at a fixed position, in order to perpetually monitor a subject(s) of monitoring. Regarding the given subject(s) of monitoring, the millimeter wave radar has its resolution of detection adjusted and set to an optimum value.
A millimeter wave radar incorporating an array antenna according to an embodiment of the present disclosure is capable of detection with a radio frequency electromagnetic wave exceeding e.g. 100 GHz. As for the modulation band in those schemes which are used in radar recognition, e.g., the FMCW method, the millimeter wave radar currently achieves a wide band exceeding 4 GHz, which supports the aforementioned Ultra Wide Band (UWB). Note that the modulation band is related to the range resolution. In a conventional patch antenna, the modulation band was up to about 600 MHz, thus resulting in a range resolution of 25 cm. On the other hand, a millimeter wave radar associated with the present array antenna has a range resolution of 3.75 cm, indicative of a performance which rivals the range resolution of conventional LIDAR. Whereas an optical sensor such as LIDAR is unable to detect a target in nighttime or bad weather as mentioned above, a millimeter wave radar is always capable of detection, regardless of daytime or nighttime and irrespective of weather. As a result, a millimeter wave radar associated with the present array antenna is available for a variety of applications which were not possible with a millimeter wave radar incorporating any conventional patch antenna.
Hereinafter, examples of monitoring systems embodying these applications will be specifically described.
[Natural Element Monitoring System]
A first monitoring system is a system that monitors natural elements (hereinafter referred to as a “natural element monitoring system”). With reference to
The natural element monitoring system 1500 is able to monitor a plurality of sensor sections 1010, 1020, etc., with the single main section 1100. When the plurality of sensor sections are distributed over a certain area, the water levels of rivers in that area can be grasped simultaneously. This allows to make an assessment as to how the rainfall in this area may affect the water levels of the rivers, possibly leading to disasters such as floods. Information concerning this can be conveyed to the distinct system 1200 (e.g., a weather observation monitoring system) via the telecommunication lines 1300. Thus, the distinct system 1200 (e.g., a weather observation monitoring system) is able to utilize the conveyed information for weather observation or disaster prediction in a wider area.
The natural element monitoring system 1500 is also similarly applicable to any natural element other than a river. For example, the subject of monitoring of a monitoring system that monitors tsunamis or storm surges is the sea surface level. It is also possible to automatically open or close the water gate of a seawall in response to a rise in the sea surface level. Alternatively, the subject of monitoring of a monitoring system that monitors landslides to be caused by rainfall, earthquakes, or the like may be the ground surface of a mountainous area, etc.
[Traffic Monitoring System]
A second monitoring system is a system that monitors traffic (hereinafter referred to as a “traffic monitoring system”). The subject of monitoring of this traffic monitoring system may be, for example, a railroad crossing, a specific railroad, an airport runway, a road intersection, a specific road, a parking lot, etc.
For example, when the subject of monitoring is a railroad crossing, the sensor section 1010 is placed at a position where the inside of the crossing can be monitored. In this case, in addition to the millimeter wave radar, the sensor section 1010 may also include an optical sensor such as a camera, which will allow a target (subject of monitoring) to be detected from more perspectives, through a fusion process based on radar information and image information. The target information which is obtained with the sensor section 1010 is sent to the main section 1100 via the telecommunication lines 1300. The main section 1100 collects other information (e.g., train schedule information) that may be needed in a more sophisticated recognition process or control, and issues necessary control instructions or the like based thereon. As used herein, a necessary control instruction may be, for example, an instruction to stop a train when a person, a vehicle, etc. is found inside the crossing when it is closed.
If the subject of monitoring is a runway at an airport, for example, a plurality of sensor sections 1010, 1020, etc., may be placed along the runway so as to set the runway to a predetermined resolution, e.g., a resolution that allows any foreign object on the runway that is 5 cm by 5 cm or larger to be detected. The monitoring system 1500 perpetually monitors the runway, regardless of daytime or nighttime and irrespective of weather. This function is enabled by the very ability of the millimeter wave radar according to an embodiment of the present disclosure to support UWB. Moreover, since the present millimeter wave radar device can be embodied with a small size, a high resolution, and a low cost, it provides a realistic solution for covering the entire runway surface from end to end. In this case, the main section 1100 keeps the plurality of sensor sections 1010, 1020, etc., under integrated management. If a foreign object is found on the runway, the main section 1100 transmits information concerning the position and size of the foreign object to an air-traffic control system (not shown). Upon receiving this, the air-traffic control system temporarily prohibits takeoff and landing on that runway. In the meantime, the main section 1100 transmits information concerning the position and size of the foreign object to a separately-provided vehicle, which automatically cleans the runway surface, etc., for example. Upon receive this, the cleaning vehicle may autonomously move to the position where the foreign object exists, and automatically remove the foreign object. Once removal of the foreign object is completed, the cleaning vehicle transmits information of the completion to the main section 1100. Then, the main section 1100 again confirms that the sensor section 1010 or the like which has detected the foreign object now reports that “no foreign object exists” and that it is safe now, and informs the air-traffic control system of this. Upon receiving this, the air-traffic control system may lift the prohibition of takeoff and landing from the runway.
Furthermore, in the case where the subject of monitoring is a parking lot, for example, it may be possible to automatically recognize which position in the parking lot is currently vacant. A related technique is described in the specification of U.S. Pat. No. 6,943,726, the entire disclosure of which is incorporated herein by reference.
[Security Monitoring System]
A third monitoring system is a system that monitors a trespasser into a piece of private land or a house (hereinafter referred to as a “security monitoring system”). The subject of monitoring of this security monitoring system may be, for example, a specific region within a piece of private land or a house, etc.
For example, if the subject of monitoring is a piece of private land, the sensor section(s) 1010 may be placed at one position, or two or more positions where the sensor section(s) 1010 is able to monitor it. In this case, in addition to the millimeter wave radar, the sensor section(s) 1010 may also include an optical sensor such as a camera, which will allow a target (subject of monitoring) to be detected from more perspectives, through a fusion process based on radar information and image information. The target information which was obtained by the sensor section 1010(s) is sent to the main section 1100 via the telecommunication lines 1300. The main section 1100 collects other information (e.g., reference data or the like needed to accurately recognize whether the trespasser is a person or an animal such as a dog or a bird) that may be needed in a more sophisticated recognition process or control, and issues necessary control instructions or the like based thereon. As used herein, a necessary control instruction may be, for example, an instruction to sound an alarm or activate lighting that is installed in the premises, and also an instruction to directly report to a person in charge of the premises via mobile telecommunication lines or the like, etc. The processing section 1101 in the main section 1100 may allow an internalized, sophisticated apparatus of recognition (that adopts deep learning or a like technique) to recognize the detected target. Alternatively, such a sophisticated apparatus of recognition may be provided externally, in which case the sophisticated apparatus of recognition may be connected via the telecommunication lines 1300.
A related technique is described in the specification of U.S. Pat. No. 7,425,983, the entire disclosure of which is incorporated herein by reference.
Another embodiment of such a security monitoring system may be a human monitoring system to be installed at a boarding gate at an airport, a station wicket, an entrance of a building, or the like. The subject of monitoring of such a human monitoring system may be, for example, a boarding gate at an airport, a station wicket, an entrance of a building, or the like.
If the subject of monitoring is a boarding gate at an airport, the sensor section(s) 1010 may be installed in a machine for checking personal belongings at the boarding gate, for example. In this case, there may be two checking methods as follows. In a first method, the millimeter wave radar transmits an electromagnetic wave, and receives the electromagnetic wave as it reflects off a passenger (which is the subject of monitoring), thereby checking personal belongings or the like of the passenger. In a second method, a weak millimeter wave which is radiated from the passenger's own body is received by the antenna, thus checking for any foreign object that the passenger may be hiding. In the latter method, the millimeter wave radar preferably has a function of scanning the received millimeter wave. This scanning function may be implemented by using digital beam forming, or through a mechanical scanning operation. Note that the processing by the main section 1100 may utilize a communication process and a recognition process similar to those in the above-described examples.
[Building Inspection System (Non-Destructive Inspection)]
A fourth monitoring system is a system that monitors or checks the concrete material of a road, a railroad overpass, a building, etc., or the interior of a road or the ground, etc., (hereinafter referred to as a “building inspection system”). The subject of monitoring of this building inspection system may be, for example, the interior of the concrete material of an overpass or a building, etc., or the interior of a road or the ground, etc.
For example, if the subject of monitoring is the interior of a concrete building, the sensor section 1010 is structured so that the antenna 1011 can make scan motions along the surface of a concrete building. As used herein, “scan motions” may be implemented manually, or a stationary rail for the scan motion may be separately provided, upon which to cause the movement by using driving power from an electric motor or the like. In the case where the subject of monitoring is a road or the ground, the antenna 1011 may be installed face-down on a vehicle or the like, and the vehicle may be allowed to travel at a constant velocity, thus creating a “scan motion”. The electromagnetic wave to be used by the sensor section 1010 may be a millimeter wave in e.g. the so-called terahertz region, exceeding 100 GHz. As described earlier, even with an electromagnetic wave over e.g. 100 GHz, an array antenna according to an embodiment of the present disclosure can be adapted to have smaller losses than do conventional patch antennas or the like. An electromagnetic wave of a higher frequency is able to permeate deeper into the subject of checking, such as concrete, thereby realizing a more accurate non-destructive inspection. Note that the processing by the main section 1100 may also utilize a communication process and a recognition process similar to those in the other monitoring systems described above.
A related technique is described in the specification of U.S. Pat. No. 6,661,367, the entire disclosure of which is incorporated herein by reference.
[Human Monitoring System]
A fifth monitoring system is a system that watches over a person who is subject to nursing care (hereinafter referred to as a “human watch system”). The subject of monitoring of this human watch system may be, for example, a person under nursing care or a patient in a hospital, etc.
For example, if the subject of monitoring is a person under nursing care within a room of a nursing care facility, the sensor section(s) 1010 is placed at one position, or two or more positions inside the room where the sensor section(s) 1010 is able to monitor the entirety of the inside of the room. In this case, in addition to the millimeter wave radar, the sensor section 1010 may also include an optical sensor such as a camera. In this case, the subject of monitoring can be monitored from more perspectives, through a fusion process based on radar information and image information. On the other hand, when the subject of monitoring is a person, from the standpoint of privacy protection, monitoring with a camera or the like may not be appropriate. Therefore, sensor selections must be made while taking this aspect into consideration. Note that target detection by the millimeter wave radar will allow a person, who is the subject of monitoring, to be captured not by his or her image, but by a signal (which is, as it were, a shadow of the person). Therefore, the millimeter wave radar may be considered as a desirable sensor from the standpoint of privacy protection.
Information of the person under nursing care which has been obtained by the sensor section(s) 1010 is sent to the main section 1100 via the telecommunication lines 1300. The main section 1100 collects other information (e.g., reference data or the like needed to accurately recognize target information of the person under nursing care) that may be needed in a more sophisticated recognition process or control, and issues necessary control instructions or the like based thereon. As used herein, a necessary control instruction may be, for example, an instruction to directly report a person in charge based on the result of detection, etc. The processing section 1101 in the main section 1100 may allow an internalized, sophisticated apparatus of recognition (that adopts deep learning or a like technique) to recognize the detected target. Alternatively, such a sophisticated apparatus of recognition may be provided externally, in which case the sophisticated apparatus of recognition may be connected via the telecommunication lines 1300.
In the case where a person is the subject of monitoring of the millimeter wave radar, at least the two following functions may be added.
A first function is a function of monitoring the heart rate and/or the respiratory rate. In the case of a millimeter wave radar, an electromagnetic wave is able to see through the clothes to detect the position and motions of the skin surface of a person's body. First, the processing section 1101 detects a person who is the subject of monitoring and an outer shape thereof. Next, in the case of detecting a heart rate, for example, a position on the body surface where the heartbeat motions are easy to detect may be identified, and the motions there may be chronologically detected. This allows a heart rate per minute to be detected, for example. The same is also true when detecting a respiratory rate. By using this function, the health status of a person under nursing care can be perpetually checked, thus enabling a higher-quality watch over a person under nursing care.
A second function is a function of fall detection. A person under nursing care such as an elderly person may fall from time to time, due to weakened legs and feet. When a person falls, the velocity or acceleration of a specific site of the person's body, e.g., the head, will reach a certain level or greater. When the subject of monitoring of the millimeter wave radar is a person, the relative velocity or acceleration of the target of interest can be perpetually detected. Therefore, by identifying the head as the subject of monitoring, for example, and chronologically detecting its relative velocity or acceleration, a fall can be recognized when a velocity of a certain value or greater is detected. When recognizing a fall, the processing section 1101 can issue an instruction or the like corresponding to pertinent nursing care assistance, for example.
Note that the sensor section(s) 1010 is secured to a fixed position(s) in the above-described monitoring system or the like. However, the sensor section(s) 1010 can also be installed on a moving entity, e.g., a robot, a vehicle, a flying object such as a drone. As used herein, the vehicle or the like may encompass not only an automobile, but also a smaller sized moving entity such as an electric wheelchair, for example. In this case, this moving entity may include an internal GPS unit which allows its own current position to be always confirmed. In addition, this moving entity may also have a function of further improving the accuracy of its own current position by using map information and the map update information which has been described with respect to the aforementioned fifth processing apparatus.
Furthermore, in any device or system that is similar to the above-described first to third detection devices, first to sixth processing apparatuses, first to fifth monitoring systems, etc., a like construction may be adopted to utilize an array antenna or a millimeter wave radar according to an embodiment of the present disclosure.
<Application Example 3: Communication System>
[First Example of Communication System]
The waveguide device and antenna device (array antenna) according to the present disclosure can be used for the transmitter and/or receiver with which a communication system (telecommunication system) is constructed. The waveguide device and antenna device according to the present disclosure are composed of layered conductive members, and therefore are able to keep the transmitter and/or receiver size smaller than in the case of using a hollow waveguide. Moreover, there is no need for dielectric, and thus the dielectric loss of electromagnetic waves can be kept smaller than in the case of using a microstrip line. Therefore, a communication system including a small and highly efficient transmitter and/or receiver can be constructed.
Such a communication system may be an analog type communication system which transmits or receives an analog signal that is directly modulated. However, a digital communication system may be adopted in order to construct a more flexible and higher-performance communication system.
Hereinafter, with reference to
With the analog to digital (A/D) converter 812, the transmitter 810A converts an analog signal which is received from the signal source 811 to a digital signal. Next, the digital signal is encoded by the encoder 813. As used herein, “encoding” means altering the digital signal to be transmitted into a format which is suitable for communication. Examples of such encoding include CDM (Code-Division Multiplexing) and the like. Moreover, any conversion for effecting TDM (Time-Division Multiplexing) or FDM (Frequency Division Multiplexing), or OFDM (Orthogonal Frequency Division Multiplexing) is also an example of encoding. The encoded signal is converted by the modulator 814 into a radio frequency signal, so as to be transmitted from the transmission antenna 815.
In the field of communications, a wave representing a signal to be superposed on a carrier wave may be referred to as a “signal wave”; however, the term “signal wave” as used in the present specification does not carry that definition. A “signal wave” as referred to in the present specification is broadly meant to be any electromagnetic wave to propagate in a waveguide, or any electromagnetic wave for transmission/reception via an antenna element.
The receiver 820A restores the radio frequency signal that has been received by the reception antenna 825 to a low-frequency signal at the demodulator 824, and to a digital signal at the decoder 823. The decoded digital signal is restored to an analog signal by the digital to analog (D/A) converter 822, and is sent to a data sink (data receiver) 821. Through the above processes, a sequence of transmission and reception processes is completed.
When the communicating agent is a digital appliance such as a computer, analog to digital conversion of the transmission signal and digital to analog conversion of the reception signal are not needed in the aforementioned processes. Thus, the analog to digital converter 812 and the digital to analog converter 822 in
In a digital communication system, in order to ensure signal intensity or expand channel capacity, various methods may be adopted. Many such methods are also effective in a communication system which utilizes radio waves of the millimeter wave band or the terahertz band.
Radio waves in the millimeter wave band or the terahertz band have higher straightness than do radio waves of lower frequencies, and undergoes less diffraction, i.e., bending around into the shadow side of an obstacle. Therefore, it is not uncommon for a receiver to fail to directly receive a radio wave that has been transmitted from a transmitter. Even in such situations, reflected waves may often be received, but a reflected wave of a radio wave signal is often poorer in quality than is the direct wave, thus making stable reception more difficult. Furthermore, a plurality of reflected waves may arrive through different paths. In that case, the reception waves with different path lengths might differ in phase from one another, thus causing multi-path fading.
As a technique for improving such situations, a so-called antenna diversity technique may be used. In this technique, at least one of the transmitter and the receiver includes a plurality of antennas. If the plurality of antennas are parted by distances which differ from one another by at least about the wavelength, the resulting states of the reception waves will be different. Accordingly, the antenna that is capable of transmission/reception with the highest quality among all is selectively used, thereby enhancing the reliability of communication. Alternatively, signals which are obtained from more than one antenna may be merged for an improved signal quality.
In the communication system 800A shown in
[Second Example of Communication System]
The azimuth of the main lobe 817 may be altered by allowing the respective phase shifters 816 to impart varying phase differences. This method may be referred to as beam steering. By finding phase differences that are conducive to the best transmission/reception state, the reliability of communication can be enhanced. Although the example here illustrates a case where the phase difference to be imparted by the phase shifters 816 is constant between any adjacent antenna elements 8151, this is not limiting. Moreover, phase differences may be imparted so that the radio wave will be radiated in an azimuth which allows not only the direct wave but also reflected waves to reach the receiver.
A method called null steering can also be used in the transmitter 810B. This is a method where phase differences are adjusted to create a state where the radio wave is radiated in no specific direction. By performing null steering, it becomes possible to restrain radio waves from being radiated toward any other receiver to which transmission of the radio wave is not intended. This can avoid interference. Although a very broad frequency band is available to digital communication utilizing millimeter waves or terahertz waves, it is nonetheless preferable to make as efficient a use of the bandwidth as possible. By using null steering, plural instances of transmission/reception can be performed within the same band, whereby efficiency of utility of the bandwidth can be enhanced. A method which enhances the efficiency of utility of the bandwidth by using techniques such as beam forming, beam steering, and null steering may sometimes be referred to as SDMA (Spatial Division Multiple Access).
[Third Example of Communication System]
In order to increase the channel capacity in a specific frequency band, a method called MIMO (Multiple-Input and Multiple-Output) may be adopted. Under MIMO, a plurality of transmission antennas and a plurality of reception antennas are used. A radio wave is radiated from each of the plurality of transmission antennas. In one example, respectively different signals may be superposed on the radio waves to be radiated. Each of the plurality of reception antennas receives all of the transmitted plurality of radio waves. However, since different reception antennas will receive radio waves that arrive through different paths, differences will occur among the phases of the received radio waves. By utilizing these differences, it is possible to, at the receiver side, separate the plurality of signals which were contained in the plurality of radio waves.
The waveguide device and antenna device according to the present disclosure can also be used in a communication system which utilizes MIMO. Hereinafter, an example such a communication system will be described.
Having received a signal from the data signal source 831, the transmitter 830 encodes the signal at the encoder 832 so that the signal is ready for transmission. The encoded signal is distributed by the TX-MIMO processor 833 between the two transmission antennas 8351 and 8352.
In a processing method according to one example of the MIMO method, the TX-MIMO processor 833 splits a sequence of encoded signals into two, i.e., as many as there are transmission antennas 8352, and sends them in parallel to the transmission antennas 8351 and 8352. The transmission antennas 8351 and 8352 respectively radiate radio waves containing information of the split signal sequences. When there are N transmission antennas, the signal sequence is split into N. The radiated radio waves are simultaneously received by the two reception antennas 8451 and 8452. In other words, in the radio waves which are received by each of the reception antennas 8451 and 8452, the two signals which were split at the time of transmission are mixedly contained. Separation between these mixed signals is achieved by the RX-MIMO processor 843.
The two mixed signals can be separated by paying attention to the phase differences between the radio waves, for example. A phase difference between two radio waves of the case where the radio waves which have arrived from the transmission antenna 8351 are received by the reception antennas 8451 and 8452 is different from a phase difference between two radio waves of the case where the radio waves which have arrived from the transmission antenna 8352 are received by the reception antennas 8451 and 8452. That is, the phase difference between reception antennas differs depending on the path of transmission/reception. Moreover, unless the spatial relationship between a transmission antenna and a reception antenna is changed, the phase difference therebetween remains unchanged. Therefore, based on correlation between reception signals received by the two reception antennas, as shifted by a phase difference which is determined by the path of transmission/reception, it is possible to extract any signal that is received through that path of transmission/reception. The RX-MIMO processor 843 may separate the two signal sequences from the reception signal e.g. by this method, thus restoring the signal sequence before the split. The restored signal sequence still remains encoded, and therefore is sent to the decoder 842 so as to be restored to the original signal there. The restored signal is sent to the data sink 841.
Although the MIMO communication system 800C in this example transmits or receives a digital signal, an MIMO communication system which transmits or receives an analog signal can also be realized. In that case, in addition to the construction of
Note that it is not an essential requirement that the plurality of transmission antennas radiate transmission waves containing respectively independent signals. So long as separation is possible at the reception antenna side, each transmission antenna may radiate a radio wave containing a plurality of signals. Moreover, beam forming may be performed at the transmission antenna side, while a transmission wave containing a single signal, as a synthetic wave of the radio waves from the respective transmission antennas, may be formed at the reception antenna. In this case, too, each transmission antenna is adapted so as to radiate a radio wave containing a plurality of signals.
In this third example, too, as in the first and second examples, various methods such as CDM, FDM, TDM, and OFDM may be used as a method of signal encoding.
In a communication system, a circuit board that implements an integrated circuit (referred to as a signal processing circuit or a communication circuit) for processing signals may be stacked as a layer on the waveguide device and antenna device according to an embodiment of the present disclosure. Since the waveguide device and antenna device according to an embodiment of the present disclosure is structured so that plate-like conductive members are layered therein, it is easy to further stack a circuit board thereupon. By adopting such an arrangement, a transmitter and a receiver which are smaller in volume than in the case where a hollow waveguide or the like is employed can be realized.
In the first to third examples of the communication system as described above, each element of a transmitter or a receiver, e.g., an analog to digital converter, a digital to analog converter, an encoder, a decoder, a modulator, a demodulator, a TX-MIMO processor, or an RX-MIMO processor, is illustrated as one independent element in
As described above, the present disclosure encompasses antenna arrays, waveguide devices, antenna devices, radars, radar systems, and communication systems as recited in the following Items.
[Item 1]
An antenna array comprising
an electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, wherein,
the electrically conductive member has a plurality of slots forming a row along a first direction;
the first electrically conductive surface of the electrically conductive member is shaped so as to define a plurality of horns each communicating with a corresponding one of the plurality of slots;
E planes of the plurality of slots are on a same plane, or on a plurality of planes which are substantially parallel to one another;
the plurality of slots include a first slot and a second slot which are adjacent to each other;
the plurality of horns include a first horn communicating with the first slot and a second horn communicating with the second slot;
in an E-plane cross section of the first horn, a length from one of two intersections between the E plane and an edge of the first slot to one of two intersections between the E plane and an edge of the aperture plane of the first horn is longer than a length from the other intersection between the E plane and the edge of the first slot to the other intersection between the E plane and the edge of the aperture plane of the first horn, the lengths extending along an inner wall surface of the first horn;
in an E-plane cross section of the second horn, a length from one of two intersections between the E plane and an edge of the second slot to one of two intersections between the E plane and an edge of the aperture plane of the second horn is equal to or less than a length from the other intersection between the E plane and the edge of the second slot to the other intersection between the E plane and the edge of the aperture plane of the second horn, the lengths extending along an inner wall surface of the second horn; and
an axis which passes through a center of the first slot and through a center of the aperture plane of the first horn and an axis which passes through a center of the second slot and through a center of the aperture plane of the second horn are oriented in different directions.
[Item 2]
The antenna array of Item 1, wherein a distance between the centers of the aperture planes of the first and second horns is shorter than a distance between centers of the first and second slots.
[Item 3]
The antenna array of Item 1 or 2, wherein each of the plurality of horns has a shape which is symmetric with respect to the E plane thereof, the E plane passing through a center of the horn.
[Item 4]
The antenna array of any of Items 1 to 3, wherein,
the plurality of slots include a third slot;
the plurality of horns include a third horn communicating with the third slot;
the first horn has a shape which is asymmetric with respect to a plane which passes through the center of the first slot and which is perpendicular to both of the E plane of the first slot and the aperture plane of the first horn;
the second horn has a shape which is asymmetric with respect to a plane which passes through the center of the second slot and which is perpendicular to both of the E plane of the second slot and the aperture plane of the second horn; and
the third horn has a shape which is symmetric with respect to a plane which passes through a center of the third slot communicating with the third horn and which is perpendicular to both of the E plane of the third slot and the aperture plane of the third horn.
[Item 5]
The antenna array of Item 4, wherein,
the third slot is adjacent to the second slot;
the plurality of slots include a fourth slot which is adjacent to the first slot, a fifth slot which is adjacent to the fourth slot, and a sixth slot which is adjacent to the fifth slot;
the plurality of horns include fourth to sixth horns respectively communicating with the fourth to sixth slots; and
the fourth to sixth horns have shapes obtained by inverting the first to third horns, respectively, with respect to a plane which extends through a midpoint between the first horn and the fourth horn and is perpendicular to the E plane thereof.
[Item 6]
The antenna array of Items 1 to 5, wherein,
the antenna array is used for at least one of transmission and reception of an electromagnetic wave of a frequency band having a center frequency f0;
an electromagnetic wave with the center frequency f0 has a free-space wavelength λ0;
in the E-plane cross section of the first horn, there is a difference of not less than λ0/32 and not more than λ0/4 between the length from the one intersection between the E plane and the edge of the first slot to the one intersection between the E plane and the edge of the aperture plane of the first horn and the length from the other intersection between the E plane and the edge of the first slot to the other intersection between the E plane and the edge of the aperture plane of the first horn, the lengths extending along the inner wall surface of the first horn; and
in the E-plane cross section of the second horn, there is a difference of not less than λ0/32 and not more than λ0/4 between the length from the one intersection between the E plane and the edge of the second slot to the one intersection between the E plane and the edge of the aperture plane of the second horn and the length from the other intersection between the E plane and the edge of the second slot to the other intersection between the E plane and the edge of the aperture plane of the second horn, the lengths extending along the inner wall surface of the second horn.
[Item 7]
The antenna array of any of Items 1 to 6, wherein, the antenna array is used for at least one of transmission and reception of an electromagnetic wave of a frequency band having a center frequency f0;
an electromagnetic wave with the center frequency f0 has a free-space wavelength λ0; and
the aperture plane of each horn has a width which is smaller than λ0 along the E plane.
[Item 8]
The antenna array of any of Items 1 to 7, wherein at least one inner wall surface extending in a direction which intersects the E plane of at least one of the plurality of horns has a projection protruding toward a central portion of the slot communicating with the at least one horn as viewed from a direction perpendicular to the aperture plane of the horn.
[Item 9]
The antenna array of any of Items 1 to 8, wherein the first electrically conductive surface of the electrically conductive member has a flat face continuing from the edge of the aperture plane or planes of a horn or horns at one end or both ends of a row constituted by the plurality of horns.
[Item 10]
The antenna array of any of Items 1 to 9, further comprising
a waveguide member provided at the rear side of the electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface,
a second electrically conductive member provided at the rear side of the electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface and a fourth electrically conductive surface on the rear side, and an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face; and the plurality of slots each oppose the waveguide face.
[Item 11]
The antenna array of any of Items 1 to 9, further comprising a hollow waveguide, wherein
the plurality of slots are connected to the hollow waveguide.
[Item 12]
The antenna array of Item 11, wherein,
at least a portion of the electrically conductive member comprises a longitudinal wall of the hollow waveguide; and the plurality of slots and the plurality of horns are provided in or on the longitudinal wall of the hollow waveguide.
[Item 13]
The antenna array of Item 11, wherein,
the hollow waveguide includes a stem and a plurality of branches emerging from the stem via at least one branching portion; and
terminal ends of the plurality of branches are respectively connected to the plurality of slots.
[Item 14]
The antenna array of any of Items 1 to 13, wherein each horn has a pyramidal shape.
[Item 15]
The antenna array of any of Items 1 to 13, wherein each horn is a box horn having an internal cavity of a rectangular solid shape or a cube shape.
[Item 16]
An antenna array comprising
an electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, wherein,
the electrically conductive member has a plurality of slots forming a row along a first direction;
the first electrically conductive surface of the electrically conductive member is shaped so as to define a plurality of horns each communicating with a corresponding one of the plurality of slots;
E planes of the plurality of slots are on a same plane, or on a plurality of planes which are substantially parallel to one another;
the plurality of horns include a first horn, a second horn, and a third horn forming a row along the first direction; and
when electromagnetic waves are supplied to first to third slots respectively communicating with the first to third horns,
three main lobes respectively radiated from the first to third horns overlap one another,
center axes of the three main lobes are oriented in respectively different directions, and
differences among the directions of the center axes of the three main lobes are smaller than a width of each of the three main lobes.
[Item 17]
A waveguide device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side;
a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface; and
a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
the second electrically conductive member includes a port at a position adjacent to one end of the waveguide member, the port communicating from the fourth electrically conductive surface to the waveguide, and
a choke structure at a position opposing the one end of the waveguide member via the port;
the choke structure includes an electrically-conductive ridge at a position adjacent to the port and includes one or more electrically conductive rods provided on the third electrically conductive surface with a gap from a farther end of the ridge from the port; and
when an electromagnetic wave propagating in the waveguide has a central wavelength λ0 in free space,
the ridge has a length equal to or greater than λ0/16 and less than λ0/4 in a direction along the waveguide.
[Item 18]
A waveguide device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side;
a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
the first electrically conductive member includes a port provided at a position opposing a portion of the waveguide face adjacent to one end of the waveguide member, the port communicating from the first electrically conductive surface to the second electrically conductive surface;
the second electrically conductive member includes a choke structure in a region containing the one end of the waveguide member;
the choke structure comprises a waveguide member end portion and one or more electrically conductive rods, the waveguide member end portion spanning from an edge of an opening of the port to an edge of the one end of the waveguide member as projected onto the waveguide face, the one or more electrically conductive rods being provided on the third electrically conductive surface with a gap from the one end of the waveguide member; and
when an electromagnetic wave propagating in the waveguide has a central wavelength λ0 in free space,
the waveguide member end portion has a length equal to or greater than λ0/16 and less than λ0/4 in a direction along the waveguide.
[Item 19]
A waveguide device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side;
a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
the second electrically conductive member includes
a port at a position adjacent to one end of the waveguide member, the port communicating from the fourth electrically conductive surface to the waveguide, and
a choke structure at a position opposing the one end of the waveguide member via the port;
the choke structure includes an electrically-conductive ridge at a position adjacent to the port and includes one or more electrically conductive rods provided on the third electrically conductive surface with a gap from a farther end of the ridge from the port;
the ridge includes a first portion adjacent to the port and a second portion adjacent to the first portion; and
a distance between the first portion and the second electrically conductive surface is longer than a distance between the second portion and the second electrically conductive surface.
[Item 20]
The waveguide device of Item 19, wherein,
the waveguide member includes a gap enlargement at a site adjacent to the port; and
a distance between the gap enlargement and the second electrically conductive surface is larger than a distance between the second electrically conductive surface and a site of the waveguide member adjoining the gap enlargement on the opposite side from the port.
[Item 21]
The waveguide device of Item 20, wherein the waveguide member has a slope at the gap enlargement.
[Item 22]
The waveguide device of any of Items 19 to 21, wherein the ridge of the choke structure has a slope at the first portion.
[Item 23]
A waveguide device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side;
a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
the first electrically conductive member includes a port provided at a position opposing a portion of the waveguide face adjacent to one end of the waveguide member, the port communicating from the first electrically conductive surface to the second electrically conductive surface;
the second electrically conductive member includes a choke structure in a region containing the one end of the waveguide member;
the choke structure comprises a waveguide member end portion and one or more electrically conductive rods, the waveguide member end portion spanning from an edge of an opening of the port to an edge of the one end of the waveguide member as projected onto the waveguide face, the one or more electrically conductive rods being provided on the third electrically conductive surface with a gap from the one end of the waveguide member;
at a site opposing the waveguide member end portion, the second electrically conductive surface of the first electrically conductive member includes a first portion adjacent to the port and a second portion adjacent to the first portion; and
a distance between the first portion and the waveguide face is longer than a distance between the second portion and the waveguide face.
[Item 24]
The waveguide device of Item 23, wherein,
the second electrically conductive surface of the first electrically conductive member includes a gap enlargement at a site adjacent to the port on a farther side from the choke structure; and
a distance between the gap enlargement and the waveguide face is longer than a distance between the waveguide face and a site of the second electrically conductive surface adjacent to the gap enlargement on an opposite side from the port.
[Item 25]
The waveguide device of Item 24, wherein the first electrically conductive member has a slope at the gap enlargement.
[Item 26]
The waveguide device of any of Items 23 to 25, wherein the waveguide member has a slope at the one end.
[Item 27]
A waveguide device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side;
a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
the second electrically conductive member includes a port communicating from the fourth electrically conductive surface to the waveguide;
the waveguide member is spatially separated into a first portion and a second portion at the port;
a portion of an inner wall of the port connects to one end of the first portion of the waveguide member;
another portion of the inner wall of the port connects to one end the second portion of the waveguide member; and
an intra-waveguide member gap defined between two opposing end faces at the one end of the first portion and the one end of the second portion of the waveguide member includes a narrow portion which is smaller in size than a gap between the portion of the inner wall of the port that connects to the first portion of the waveguide member and the other portion of the inner wall of the port that connects to the second portion of the waveguide member.
[Item 28]
The waveguide device of Item 27, wherein a cross section of the port taken orthogonal to a center axis of the port has an H-shape.
[Item 29]
The waveguide device Item 27 or 28, wherein the narrow portion reaches the waveguide face of the waveguide member.
[Item 30]
The waveguide device of any of Items 27 to 29, wherein the narrow portion reaches inside the port.
[Item 31]
An array antenna device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, the first electrically conductive member having a plurality of slots;
a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
the second electrically conductive member includes a port communicating from the fourth electrically conductive surface to the waveguide;
on the second electrically conductive surface, a first slot and a second slot which are adjacent to each other among the plurality of slots are at symmetric positions with respect to a center of the port;
the waveguide member includes a pair of impedance matching structures adjoining the port, each of the pair of impedance matching structures having a flat portion adjoining the port and a dent adjoining the flat portion, and partly opposes one of the first and second slots.
[Item 32]
The array antenna device of Item 31, wherein, when a signal wave propagating in the waveguide has a central wavelength λ0 while propagating in a vacuum, a length of the flat portion along a direction that the waveguide member extends is longer than λ0/4, and a length of the dent along the direction that the waveguide member extends is shorter than λ0/4.
[Item 33]
The array antenna device of Item 32, wherein a distance on the second electrically conductive surface from a center of the first slot to a center of the second slot is shorter than 2λ0, and longer than λ0.
[Item 34]
The array antenna device of any of Items 31 to 33, wherein at least a portion of the dent of each of the pair of impedance matching structures opposes one of the first and second slots.
[Item 35]
The array antenna device of any of Items 31 to 34, wherein the plurality of slots include a third slot which is adjacent to the first slot and a fourth slot which is adjacent to the second slot, and the third and fourth slots are at symmetric positions with respect to the center of the port on the second electrically conductive surface.
[Item 36]
The array antenna device of Item 35, wherein,
at least one of a distance from the second electrically conductive surface to the waveguide face and a width of the waveguide face varies along the waveguide; and on the second electrically conductive surface, a distance from a center of the first slot to a center of the third slot is shorter than a distance from the center of the first slot to a center of the second slot.
[Item 37]
The array antenna device of Item 35 or 36, wherein, on the second electrically conductive surface, a distance from a center of the first slot to a center of the third slot is equal to a wavelength, as taken within the waveguide, of a signal wave propagating in the waveguide.
[Item 38]
An array antenna device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side;
a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
the second electrically conductive member includes a port communicating from the fourth electrically conductive surface to the waveguide;
the waveguide member is spatially separated into a first portion and a second portion at the port;
a portion of an inner wall of the port connects to one end of the first portion of the waveguide member;
another portion of the inner wall of the port connects to one end the second portion of the waveguide member;
a distance between two opposing end faces at the one end of the first portion and the one end of the second portion of the waveguide member is different from a distance between the portion of the inner wall of the port that connects to the first portion of the waveguide member and the other portion of the inner wall of the port that connects to the second portion of the waveguide member.
[Item 39]
The array antenna device of Item 38, wherein a cross section of the port taken orthogonal to a center axis of the port has an H-shape.
[Item 40]
The array antenna device of Item 38 or 39, wherein the first portion and the second portion of the waveguide member each include an impedance matching structure adjoining the port, the impedance matching structure having a flat portion adjoining the port and a dent adjoining the flat portion.
[Item 41]
An array antenna device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, the first electrically conductive member having a plurality of slots;
a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
the second electrically conductive member includes a port communicating from the fourth electrically conductive surface to the waveguide;
the plurality of slots opposes the waveguide face;
on the second electrically conductive surface, a first slot and a second slot which are adjacent to each other among the plurality of slots are at symmetric positions with respect to a center of the port;
the first electrically conductive surface of the first electrically conductive member is shaped so as to define a plurality of horns respectively communicating with the plurality of slots; and
among the plurality of horns, a distance between centers of the openings of two adjacent horns is shorter than a distance on the second electrically conductive surface from a center of the first slot to a center of the second slot.
[Item 42]
The array antenna device of Item 41, wherein the plurality of slots include a third slot which is adjacent to the first slot and a fourth slot which is adjacent to the second slot, and the third and fourth slots are at symmetric positions with respect to the center of the port on the second electrically conductive surface.
[Item 43]
The array antenna device of Item 41 or 42, wherein each of the plurality of horns has a shape which is asymmetric with respect to a plane that passes through the center of a slot communicating with the horn and is orthogonal to both of the second electrically conductive surface and the waveguide.
[Item 44]
The array antenna device of Item 42, wherein, on the second electrically conductive surface, a distance from a center of the first slot to a center of the third slot is equal to a wavelength, as taken within the waveguide, of a signal wave propagating in the waveguide.
[Item 45]
The array antenna device any of Items 41 to 44, wherein at least one of a distance from the second electrically conductive surface to the waveguide face and a width of the waveguide face varies along the waveguide.
[Item 46]
An array antenna device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side;
a waveguide member provided at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face of a stripe shape that opposes the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
the second electrically conductive member includes
a port at a position adjacent to one end of the waveguide member, the port communicating from the fourth electrically conductive surface to the waveguide, and
a choke structure at a position opposing the one end of the waveguide member via the port;
the choke structure includes a first portion adjacent to the port and a second portion adjacent to the first portion; and
a distance between the first portion and the second electrically conductive surface is longer than a distance between the second portion and the second electrically conductive surface.
[Item 47]
An array antenna device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, the first electrically conductive member having 2N (where N is an integer of 2 or greater) ports;
a waveguide member at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face opposing the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, and the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide in a gap between the second electrically conductive surface and the waveguide face;
via combinations among a plurality of T-branching portions, the waveguide member branches from one stem into 2N waveguide terminal sections, the 2N ports respectively opposing the 2N waveguide terminal sections,
at least one of the 2N waveguide terminal sections has a shape which is different from the shape of another.
[Item 48]
The array antenna device of Item 47, wherein, among the 2N waveguide terminal sections, at least two waveguide terminal sections that are located central have a shape which is different from a shape of at least two waveguide terminal sections located outward of the two waveguide terminal sections.
[Item 49]
The array antenna device of Item 48, wherein, N≥3 is satisfied; and
[Item 50]
The array antenna device of any of Items 47 to 49, wherein,
N=3 is satisfied; and
[Item 51]
The array antenna device of Item 50, wherein, among the eight waveguide terminal sections, four waveguide terminal sections located central have a shape which is different from a shape of four waveguide terminal sections located outward of the four waveguide terminal sections.
[Item 52]
The array antenna device of Item 51, wherein,
each of the eight waveguide terminal sections has a bend where the waveguide terminal section is connected to the second branch; and
the bends of the four waveguide terminal sections located central are dented.
[Item 53]
The array antenna device of Item 51 or 52, wherein the bends of the four waveguide terminal sections located outward of the four waveguide terminal sections located central each have a bump.
[Item 54]
The array antenna device of any of Items 57 to 53, wherein the second electrically conductive member has a fourth electrically conductive surface on the rear side, and, at a position adjacent to one end of the stem of the waveguide member, the second electrically conductive member has a port communicating from the fourth electrically conductive surface to the waveguide.
[Item 55]
An array antenna device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side;
a waveguide member at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face opposing the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, and the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor being provided on at least one of the second electrically conductive surface and the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
via combinations among a plurality of T-branching portions, the waveguide member branches from one stem into 2N (where N is an integer of 2 or greater) waveguide terminal sections;
on a stem portion adjacent to each of the plurality of T-branching portions, the waveguide member includes a plurality of impedance transforming sections to increase a capacitance of the waveguide; and
among the plurality of impedance transforming sections, a length of a first impedance transforming section in a direction along the waveguide is shorter than a length of a second impedance transforming section in a direction along the waveguide, the first impedance transforming section being relatively far from the waveguide terminal section, the second impedance transforming section being relatively close to the waveguide terminal section.
[Item 56]
The array antenna device of Item 55, wherein,
N=3 is satisfied; and
the plurality of T-branching portions include a first branching portion at which the stem of the waveguide member branches into two first branches, two second branching portions at each of which each first branch branches into two second branches, and four third branching portions at each of which each second branch branches into two third branches, the eight third branches functioning as the waveguide terminal sections.
[Item 57]
The array antenna device of Item 56, wherein the first impedance transforming section is located at the first branch, and the second impedance transforming section is located at the second branch.
[Item 58]
The array antenna device of any of Items 55 to 57, wherein,
each of the first impedance transforming section and the second impedance transforming section includes
a first transforming subsection being adjacent to one of the plurality of T-branching portions and having a constant height or width, and
a second transforming subsection adjoining the first transforming subsection on an opposite side from the one of the plurality of T-branching portions and having a constant height or width; and
a distance between the waveguide face and the second electrically conductive surface at the first transforming subsection is smaller than a distance between the waveguide face and the second electrically conductive surface at the second transforming subsection, or a width of the waveguide face at the first transforming subsection is larger than a width of the waveguide face at the second transforming subsection.
[Item 59]
The array antenna device of Item 58, wherein, in a direction along the waveguide, the first transforming subsection of the first impedance transforming section is shorter than the first transforming subsection of the second impedance transforming section.
[Item 60]
The array antenna device of Item 58 or 59, wherein,
in a direction along the waveguide, the first transforming subsection of the first impedance transforming section is shorter than the second transforming subsection of the first impedance transforming section; and
in a direction along the waveguide, the first transforming subsection of the second impedance transforming section is longer than the second transforming subsection of the second impedance transforming section.
[Item 61]
An array antenna device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side;
a waveguide member at the rear side of the first electrically conductive member, the waveguide member having an electrically-conductive waveguide face opposing the second electrically conductive surface, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member provided at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface, and a fourth electrically conductive surface on the rear side; and
an artificial magnetic conductor extending on both sides of the waveguide member, the artificial magnetic conductor having a plurality of electrically conductive rods on the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
the second electrically conductive member includes
the plurality of electrically conductive rods include at least two rows of electrically conductive rods that are arrayed on both sides of the waveguide member and extending along the waveguide member; and,
as viewed from a normal direction of the third electrically conductive surface,
the rectangular hollow-waveguide has a rectangular shape which is defined by a pair of longer sides and a pair of shorter sides orthogonal to the longer sides, one of the pair of longer sides being in contact with the one end of the waveguide member, and
a length of each longer side of the rectangular hollow-waveguide is longer than twice a shortest distance between centers of the at least two rows of electrically conductive rods, and shorter than 3.5 times the shortest distance between the centers.
[Item 62]
The array antenna device of Item 61, wherein a length of each shorter side of the rectangular hollow-waveguide is shorter than 1.5 times the shortest distance between the centers of.
[Item 63]
An array antenna device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, the first electrically conductive member having a plurality of slots;
a waveguide member at the rear side of the first electrically conductive member, having an electrically-conductive waveguide face in a stripe shape opposing the second electrically conductive surface and at least one of the plurality of slots, the waveguide member extending in a manner of following along the second electrically conductive surface; and
a second electrically conductive member at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, and the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface; and
an artificial magnetic conductor extending on both sides of the waveguide member and being provided on the third electrically conductive surface, the artificial magnetic conductor having a plurality of electrically conductive rods on the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
at least one of a distance from the second electrically conductive surface to the waveguide face and a width of the waveguide face varies along the waveguide;
among the plurality of electrically conductive rods, a plurality of first electrically conductive rods adjacent to the waveguide member are in a periodic array with a first period in a direction along the waveguide; and
among the plurality of electrically conductive rods, a plurality of second electrically conductive rods not adjacent to the waveguide member are in a periodic array with a second period in a direction along the waveguide, the second period being longer than the first period.
[Item 64]
The array antenna device of Item 63, wherein, in a direction along the waveguide, a width of each first electrically conductive rod is shorter than a width of each second electrically conductive rod.
[Item 65]
The array antenna device of Item 64, wherein, in a direction along the waveguide, an interval between two adjacent first electrically conductive rods is equal to an interval between two adjacent second electrically conductive rods.
[Item 66]
The array antenna device of any of Items 63 to 65, wherein,
when a signal wave propagating in the waveguide has a central wavelength λ0 while propagating in a vacuum,
on a plane which is parallel to the second electrically conductive member, each of the plurality of first electrically conductive rods has a width less than λ0/4 as taken along a direction perpendicular to a direction along the waveguide.
[Item 67]
The array antenna device of Item 66, further comprising
a further waveguide member adjacent to the plurality of second electrically conductive rods, wherein
a distance between each of the plurality of first electrically conductive rods and the waveguide member is longer than a distance between each of the plurality of second electrically conductive rods and the further waveguide member.
[Item 68]
The array antenna device of Item 63, wherein,
each of the plurality of first electrically conductive rods and each of the plurality of second electrically conductive rods have prismatic shapes; and
as viewed from a normal direction of the third electrically conductive surface, each of the plurality of first electrically conductive rods is a non-square whose polygonal side in a direction along the waveguide is longer than another polygonal side, and each of the plurality of second electrically conductive rods is a square.
[Item 69]
An array antenna device comprising:
a first electrically conductive member having a first electrically conductive surface on a front side and a second electrically conductive surface on a rear side, the first electrically conductive member having a plurality of slots;
a waveguide member at the rear side of the first electrically conductive member, having an electrically-conductive waveguide face in a stripe shape opposing the second electrically conductive surface and at least one of the plurality of slots, the waveguide member extending in a manner of following along the second electrically conductive surface;
a second electrically conductive member at the rear side of the first electrically conductive member, the second electrically conductive member supporting the waveguide member, and the second electrically conductive member having a third electrically conductive surface on the front side that opposes the second electrically conductive surface; and
an artificial magnetic conductor extending on both sides of the waveguide member and being provided on the third electrically conductive surface, the artificial magnetic conductor having a plurality of electrically conductive rods on the third electrically conductive surface, wherein,
the second electrically conductive surface, the waveguide face, and the artificial magnetic conductor define a waveguide extending in a gap between the second electrically conductive surface and the waveguide face;
in a plane which is parallel to the second electrically conductive member, a first direction is defined as a direction extending along the waveguide, and a second direction is defined perpendicular to the first direction; and
among the plurality of electrically conductive rods, a group of rods adjacent to the waveguide member each have a dimension along the first direction which is larger than a dimension along the second direction.
[Item 70]
The array antenna device of Item 69, wherein, at least a portion of the waveguide member is surrounded by plural rows of rods provided along the first direction, the plural rows of rods including the group of rods adjacent to the waveguide member, and electrically conductive rods in the plural rows of rods have identical dimensions.
[Item 71]
The array antenna device of Item 70, wherein,
the second electrically conductive member has a further waveguide member thereon, the further waveguide member being different from the waveguide member;
the second electrically conductive surface, a waveguide face of the further waveguide member, and the artificial magnetic conductor define a further waveguide in a gap between the second electrically conductive surface and the waveguide face of the further waveguide member;
the plurality of electrically conductive rods include a first rod group and a second rod group, the first rod group being the group of rods adjacent to the waveguide member, and the second rod group being adjacent to the further waveguide member;
at least a portion of the further waveguide member is surrounded by plural rows of rods including the second rod group, the plural rows of rods being provided along the further waveguide; and
an interval between two adjacent electrically conductive rods in the first rod group is equal to an interval between two adjacent electrically conductive rods in the second rod group.
[Item 72]
An antenna device comprising:
the waveguide device of any of Items 1 to 30; and
at least one antenna element connected to the waveguide device.
[Item 73]
A radar comprising:
an antenna array of any of Items 1 to 16; and
a microwave integrated circuit connected to the antenna array.
[Item 74]
A radar comprising:
the antenna device of Item 72; and
a microwave integrated circuit connected to the antenna device.
[Item 75]
A radar comprising:
the array antenna device of any of Items 31 to 71; and
a microwave integrated circuit connected to the array antenna device.
[Item 76]
A radar system comprising:
the radar of any of Items 73 to 75; and
a signal processing circuit connected to the microwave integrated circuit of the radar.
[Item 77]
A wireless communication system comprising:
the antenna array of any of Items 1 to 16; and
a communication circuit connected to the antenna array.
[Item 78]
A wireless communication system comprising:
the antenna device of Item 72; and
a communication circuit connected to the antenna device.
[Item 79]
A wireless communication system comprising:
the array antenna device of any of Items 31 to 71; and
a communication circuit connected to the array antenna device.
While the present invention has been described with respect to exemplary embodiments thereof, it will be apparent to those skilled in the art that the disclosed invention may be modified in numerous ways and may assume many embodiments other than those specifically described above. Accordingly, it is intended by the appended claims to cover all modifications of the invention that fall within the true spirit and scope of the invention.
This application is based on Japanese Patent Application No. 2016-075684 filed Apr. 5, 2016, the entire contents of which are hereby incorporated by reference.
A waveguide device and an antenna device according to the present disclosure are usable in any technological field that makes use of an antenna. For example, they are available to various applications where transmission/reception of electromagnetic waves of the gigahertz band or the terahertz band is performed. In particular, they are suitably used in onboard radar systems, various types of monitoring systems, indoor positioning systems, and wireless communication systems where downsizing is desired.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2016-075684 | Apr 2016 | JP | national |
This is a continuation of International Application No. PCT/JP2017/014182, with an international filing date of Apr. 5, 2017, which claims priority of Japanese Patent Application No. 2016-075684 filed Apr. 5, 2016, the entire contents of which are hereby incorporated by reference.
| Number | Name | Date | Kind |
|---|---|---|---|
| 20070139287 | Inomata | Jun 2007 | A1 |
| 20110181373 | Kildal | Jul 2011 | A1 |
| 20130321229 | Klefenz | Dec 2013 | A1 |
| Entry |
|---|
| Kirino et al., “Waveguide Device and Antenna Array”, U.S. Appl. No. 16/150,385, filed Oct. 3, 2018. |
| Number | Date | Country | |
|---|---|---|---|
| 20200176884 A1 | Jun 2020 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 16150385 | Oct 2018 | US |
| Child | 16780944 | US | |
| Parent | PCT/JP2017/014182 | Apr 2017 | US |
| Child | 16150385 | US |
