Patent Grant
7561109
The present invention relates to a reconfigurable antenna using addressable pixel elements.
In general, it is possible for an antenna to be made of conductive paths separated from a ground plane by a dielectric space. Such antennas can be built as a patch array with operational frequency, main beam direction and even main beam shape by printing a pattern of the transmission lines, power dividers and patch antennas on a surface above a dielectric.
However, in the past, the method of rapidly reconfiguring these types of antennas has been very restrictive. Typically, a set of radiating elements was connected to a transmission line with amplitude and phase shift elements embedded in the line. An alternative technique has been to use antenna modules with embedded phase and gain characteristics. Both of theses designs suffer from limitations due to the fixed geometry of the array of radiating elements and the configuration of the transmission lines.
Therefore, there is a need for an antenna that can be rapidly reconfigured to change its operational frequency band, its pointing angle, gain, bandwidth and its polarization in less than a millisecond. This patent describes a method for rapid reconfiguration through the use of small conductive segments, or pixel elements, to accomplish these changes.
According to the present invention, an antenna array made up of a grid of small addressable conductive segments, or pixel elements, affixed to an array of movable shaped pistons is presented. The small pixel elements can be activated in less than a millisecond to form patterns that create an array of patch antennas and associated transmission lines. The antenna array and transmission line patterns can be formed using small shaped movable pistons. Each piston comprises a handle, a bottom conductive segment affixed to the top of the handle, a dielectric segment affixed to the uppermost surface of the bottom conductive segment, and a top conductive segment affixed to the uppermost surface of the dielectric segment. The pistons can be individually addressed to be on or off and controller by a two-dimensional actuator. When the pistons are in the on, or up, position, the top conductive segments form the transmission line and antenna array patterns, the dielectric segment becomes a dielectric space and the bottom conductive segment forms a ground plane. When the piston is in the off, or down, position, the top conductive segment becomes part of the ground plane.
In accordance with one embodiment of the present invention, the top conductive segments can be triangles, squares, hexagons, or any other suitable shape.
Accordingly, it is a feature of the embodiments of the present invention to be able to rapidly reconfigure the characteristics of an antenna in less than a millisecond. Other features of the embodiments of the present invention will be apparent in light of the description of the invention embodied herein.
The following detailed description of specific embodiments of the present invention can be best understood when read in conjunction with the following drawings, where like structure is indicated with like reference numerals and in which:
In the following detailed description of the embodiments, reference is made to the accompanying drawings that form a part hereof, and in which are shown by way of illustration, and not by way of limitation, specific embodiments in which the invention may be practiced. It is to be understood that other embodiments may be utilized and that logical, mechanical and electrical changes may be made without departing from the spirit and scope of the present invention.
According to the present invention, an antenna array can be built to be electronically configured and reconfigured in less than a millisecond. The transmission lines can be modified to steer the beam and the patch geometry can be modified to shift the operational frequency. The number, disposition, shape, size and feed point of the patches can be rapidly modified to change the array shape and gain as well as the polarization. In a swept-frequency radar embodiment, the resonant frequency of the antenna array can be tracked with the instantaneous frequency of the radar. Further, since the antenna can be half-duplex, the antenna can switch from the desired transmit characteristic to the desired receive characteristic as needed.
The transmission lines (e.g., striplines and microstrips) and antenna (e.g., patches or other radiating structures) can be formed, pixel by pixel, by moving an array of shaped pistons into conductive patterns. The conductive patterns can be formed using conductive particles, or pixel elements, individually attached to the uppermost surface of the array of pistons. The individual pistons in the array can be moved, or actuated, from a ground plane (i.e., the “off” state) to a predetermined distance over the ground plane (i.e., the “on” state) by a two-dimensional actuator. The ground plane can be any grounded surface, planar or non-planar. Each pixel element on the individual pistons can be individually addressed to be either “on” of “off” by the two-dimensional actuator.
This embodiment, which may be referred to as a “pixel-on-a-shaft,” is illustrated in
In this embodiment, when the piston 1000 is down, or in the “off” position, the top conductive segment 1010 becomes an extension of a ground plane. When the piston 1000 is actuated to move up, or in the “on” position, the top conductive segment 1010 can be one of the pixel elements that becomes part of the antenna array or transmission line, the dielectric segment 1020 forms part of the dielectric space, and the bottom conductive segment 1030 becomes an extension of the ground plane. The each individual piston in the array of pistons 1000 can be individually addressable and controllable by the two-dimensional actuator. Each piston 1000 can be controlled to move, or actuate, based on a actuator command. The piston 1000 can be actuated magnetically using a solenoid, capacitively, hydraulically using air or fluid pressure, mechanically, or by any other suitable method.
Although the present invention has been described as moving the array of pixel element pistons up and down, it should be understood that the antenna arrays and transmission lines themselves can be in any suitable orientation. It is possible to position the antenna array and the transmission lines on their sides as well as upside down. The term “up” refers to moving the pixel element piston from the ground plane to a predetermined distance over the ground plane. Likewise, the term “down” refers to the pixel element piston moving from the predetermined distance towards the ground plane. Additionally, for the purposes of describing and defining the present invention, formation of a material “on” a layer refers to formation in contact with a surface of the layer. Formation “over” a layer refers to formation above or in contact with a surface of the layer.
The geometry of the top conductive segment can be nearly any shape. The shape of the top conductive segment helps determine the nature shape of the bends and interconnects that can be created by the antenna array patterns. For example, in one embodiment, the top conductive segment can be a 45-45-90 degree triangle. This shape can allow for 45 degree and 90 degrees turns more easily. In another embodiment, the top conductive segment can be square. This shape can allow for 90 degree turns and can make interconnects simple and effective. In yet another embodiment, the top conductive segment may be a hexagon. This shape can allow for 30 and 60 degree turns to be more effective and efficient. In still another embodiment, the top conductive segment can be a shape that “tiles the plane” of the antenna array. This top conductive segment shape can be optimized for improved geometrical flexibility and pixel-to-pixel capacitance. Additionally, the individuals top conductive segments can be a variety of different shapes, depending on whether the top conductive segments are to form an antenna element, a transmission line, a power splitter, or any other suitable application known in the art. Referring to
However, the size of the wavelength of the electromagnetic signal used by the antenna array can be a design constraint and should be taken into consideration. For example, the pixel element cannot be too large or the resulting transmission line can be potentially multimode and the structural control can be too limited. On the other hand, if the pixel element is too small, it can be difficult to control. Therefore, pixel element sizes of about 1/10 of a wavelength have been shown to be effective.
The antenna characteristics can be easily and quickly modified using this invention. For example, the direction of the antenna array beam can be determined by the phase distribution on the antenna array. Alternatively, the direction of the antenna beam can be determined by the differential phase or time delay along the transmission line. The location of the feed point can be shifted to shift the differential phase or time and, therefore, the main beam direction. The beamwidth can be determined by the size of the array and by the distribution of amplitude over the array. The beamwidth can be controlled using the pixel-based transmission lines. Polarization can be determined by how the antenna pixel elements are fed and by the geometry of the antenna pixel elements.
The frequency of operation of the antenna can be determined by the feed point and the size of the antenna. The size of the pixel-generated antennas, the number of array elements, and the power distribution over the array can be dynamically adjusted to yield the desired operational frequency.
Further, multiple antennas may use a single aperture. There is no electromagnetic limit to the number of feed points in the array aperture. It possible to have several feed points as well as several types of feeds (e.g., edge and thru-ground). Because of this, multiple radio/radar systems can use the same aperture.
Power distribution can be achieved by using directional couplers. Directional couples can be created by programming the geometry of the feed lines as is known in the art. Alternatively, power distribution can be achieved by using multiple transmission line impedance. The impedance of a transmission line can be controlled by the changing the width of the transmission line. For example, two transmission lines can be connected together so that a good impedance match can be achieved. Pixel element transmission lines can be created with various widths and thus various impedances. A single transmission line (i.e., the input) can be connected to two other transmission lines (i.e., the output) to form an effective feed system for a desired array antenna.
Additionally, stub tuning concepts can be used to further optimize the performance of the antenna array. Small stubs can be attached to the transmission lines as known in the art to tune components of the antenna arrays and to improve the feed point impedance match.
To feed the antenna from the edge, a coaxial to edge launch can be used to connect the antenna to the edge. Edge launch techniques and/or techniques that are known in the art can be used to excite the transmission edge. To feed the antennas from below the ground plane (i.e., away from the edge), techniques known in the art to feed transmission lines from below the ground plane can be used.
In summary, patterns can be generated on the face of specialized panels to create antenna arrays and transmission lines. The antennas can be operated at nearly any frequency and with antenna characteristics (e.g., gain, beam direction, beam width, polarization, etc.) that can be changed in less than a millisecond. Such an antenna can be used on space vehicles, aircraft and ground vehicles. In addition, such an antenna can be useful for any application where space and weight are limited and the need for communication, navigation and sensing are high. The programmability of the antenna characteristics means that such a panel antenna can be usable for many applications.
It is noted that terms like “preferably,” “commonly,” and “typically” are not utilized herein to limit the scope of the claimed invention or to imply that certain features are critical, essential, or even important to the structure or function of the claimed invention. Rather, these terms are merely intended to highlight alternative or additional features that may or may not be utilized in a particular embodiment of the present invention.
For the purposes of describing and defining the present invention it is noted that the term “substantially” is utilized herein to represent the inherent degree of uncertainty that may be attributed to any quantitative comparison, value, measurement, or other representation. The term “substantially” is also utilized herein to represent the degree by which a quantitative representation may vary from a stated reference without resulting in a change in the basic function of the subject matter at issue.
Having described the invention in detail and by reference to specific embodiments thereof, it will be apparent that modifications and variations are possible without departing from the scope of the invention defined in the appended claims. More specifically, although some aspects of the present invention are identified herein as preferred or particularly advantageous, it is contemplaned that the present invention is not necessarily limited to these preferred aspects of the invention.
This application claims the benefit of U.S. Provisional Application Ser. No. 60/890,224 (OSU 0051 MA), filed Feb. 16, 2007. This Application is related to U.S. patent application Ser. No. 12/032,261 (OSU 0051a PA), filed Feb. 15, 2008 and Ser. No. 12/032,265 (OSU 0051b PA), filed Feb. 15, 2008.
The U.S. Government has a paid-up license in this invention and the right in limited circumstances to require the patent owner to license others on reasonable terms as provided for by the terms of contract No. W9113M-04-P-0061 awarded by U.S. Army Space and Missile Defense Command.
| Number | Name | Date | Kind |
|---|---|---|---|
| 7046198 | Sakiyama et al. | May 2006 | B2 |
| 7250909 | Fujishima et al. | Jul 2007 | B2 |
| 7471247 | Saily et al. | Dec 2008 | B2 |
| Number | Date | Country | |
|---|---|---|---|
| 20080198074 A1 | Aug 2008 | US |
| Number | Date | Country | |
|---|---|---|---|
| 60890224 | Feb 2007 | US |
