Patent Grant
9385426
The invention refers to passive ultra-high frequency radiowave imaging devices and has been designed for quick formation of radio-thermal images of objects. The method and its implementing antenna can be used, in particular, for formation of radio-thermal images of human body for the purposes of thermometric medical diagnosis, or in the process of customs inspection with the purpose of revealing various objects that may be hidden on human body under clothing.
Presently ultra-high frequency radiometric methods, based on the dependence of the intensity of own radio-thermal radiation of the objects on their physical and chemical parameters, have become widely popular for remote sensing of various media. One of the primary tasks during ultra-high frequency (UHF) radiometric observations is to measure and register the spatial distribution of the intensity of radio-thermal radiation emitted by the object, which is characterized by its brightness temperature Tb. In many cases the data concerning, spatial distribution of brightness temperature for objects under investigation can be best represented by two-dimensional radio-thermal images, thereat, the two coordinates of the image correspond to spatial coordinates of the observation field, and brightness or hue of the unitary element of the image characterize the intensity of radio-thermal radiation in accordance with the established scale of brightness temperatures. At that, the higher is radiometric accuracy and spatial resolution capability of the radiometric system while generating radio-thermal images, or in other words, the higher is reproduction accuracy of spatial inhomogenuities (relief) of measured radio-thermal fields, the higher will be the efficiency of using the generated radio-thermal images for various applications, among which, in particular, are the following:
The advantages of millimeter-wave radio imaging systems are high spatial resolution, combined with relatively small dimension of reception antennas, lack of electromagnetic emissions, which may negatively influence the personnel and other people, lack of dependence of the response signal intensity from distance, in the mean time, present technical limitations do not allow full implementation of all potential capabilities of such systems. Among such limitations are complexity and high cost of the system, relatively small observation angles and slowness of image generation which, in certain cases, are insufficient for resolution of above mentioned problems.
A series of technical solutions are known for SHF radiometric systems (see for example, Goldsmith P. P., Huguenin G. R., Kapitzky J. Focal Plane Imaging Systems for Millimeter Wavelengths//IEEE Transactions on Microwave Theory and Techniques, v. MTT-41 No. 10, October 1985, pp. 1864-1675), for which the established observation field is periodically scanned during generation of images:
The disadvantages of singular beam DPA image generation scheme are the following:
Shortcomings of systems with beam-forming matrices in SHF band include the complexity of placing a large number of exciters (measurement channels) in the focal plane of the antenna when dimensions of unitary exciter are physically limited, problems related to construction of beam-forming matrices with spatially solid overlapping beams during construction of highly directed antennae, as well as the high total cost of the systems, related to the square law increase of the number of receiving channel depending on N2 the number of picture elements N on each coordinate. Thereat, each of the mentioned channels should contain a full set of elements common to ultra-high frequency radio-thermal radiation receivers. There are also other methods for generation of radio-thermal images, which combine characteristics of the beam-forming matrices method with the principles of serial spatial retargeting of the group DPA created by the beam-forming matrix, in this case the number of receivers in the system can foe reduced to a technically end economically acceptable figure, but other technical issues would appear, particularly related to the need of fast retargeting group DPA positions in the sector of observation angles.
One of the perspective methods for generation of radio-thermal images in radiowave imaging systems is through the use of scanning antennae based on the effects of transformation of volume waves into surface waves in open electrodynamic structures, which were first researched over 30 years ago (Andrenko S. D., Devyatkov N. D., Shestopalov V. P.—Antenna array of millimeter range//Doklady Akademii nauk USSR, 1978, v. 240, No 6.—P. 1340-1343, Shestopalov V. P., Andrenko S. D., Belyaev V. G., Sidorenko Yu. B., Provalov S. A. Peretvorennya milimetrovikh i submilimetrovikh poverkhnevikh elekromagnitnikh khvil v obyemni i vikoristannya cyogo yavischa u fizici i tekhnici//Naukovi oglyadi i povidomlennya, Visnik A N Ukrainskoy R S R, No 1 Sichen, 1977—S. 8-21). Such antennae usually contain a linear or planar dielectric waveguide, a scattering diffraction grating, placed in its direct proximity, as well as elements to provide concentration of electromagnetic energy and its transmission to the input of radiometric receiver.
There are known systems and methods, for example as disclosed in U.S. Pat. No. 5,933,120, for generation of images based on diffraction gratings including among their primary elements a spindle arrangement to define the axis of rotation, a waveguide arrangement linked to the spindle arrangement and containing the first linear dielectric waveguide, defining the first axis perpendicular to the rotation axis, diffraction grating arrangement, containing numerous sectors, and each sector from the mentioned array contains a different in its period conducting diffraction grating, thereat, the changing period of the diffraction grating is a function of angle set out while rotating the grating point to the rotation axis, and grating plane is perpendicular to the rotation axis. At that this system and the method provide advantages, the essence of which is that the image may be quickly generated with the help of inexpensive radiometric system.
Among the advantages of mentioned systems and methods of their implementation is the possibility for generation of two-dimensional radio-thermal images through one single receiver, through provision of radial movement of the beam from center to the circumference of cone-shaped sector of observation angles, which is achieved by isochronous unidirectional circular movement of the control elements of the antenna. Thereat sign-variable momentums of inertia are eliminated and, as a result, the speed of image generation is increasing, reaching dozens of images per second.
In the mean time, significant disadvantages are inherent to the mentioned systems and methods of implementation.
The first disadvantage is the need of simultaneous rotation, with different velocities, of both dielectric waveguide arrangement with the receiver element and the disc-shaped diffraction grating. Rotation velocity of the dielectric waveguide arrangement defines the image generation speed; rotation velocity of the grating defines the radial component of the speed of movement of the beam in space. Thereat rotation speed of the grating significantly exceeds rotation speed of the dielectric waveguide arrangement and, with high spatial resolution of the antenna, may reach several tens of thousands revolutions per minute. Although such revolution speeds can be achieved technically, this makes the device significantly complicated. The dimensions of s grating unit, which are quite large, define the dimensions of the receiving aperture of the antenna and spatial resolution of the radiowave imaging system. While rotating at high-speed. In essence, it turns into a gyroscopic device which strives to maintain its orientation in the space and thus, on the account of emerging significant mechanical momentums, preventing the change of this spatial orientation, that is, changing the position of the antenna while reviewing the space. Therefore such systems of image generation can be used, first of all, for construction of images while maintaining a stationary spatial position of the sector of observation angles. In order to suppress higher types of electromagnetic oscillations in dielectric waveguides the dimensions of its cross-section should be consistent with the length of received waves. In millimeter range if constitutes just a few millimeters, which results in significant flexibility of the waveguide. While the grating and waveguide are moving relative to each other, provision of permanently fixed distance (gap) between them is one technical problem. This gap is known to define the basic energy parameters of the electrodynamic system of the antenna—the transformation coefficient of spatial electromagnetic wave into surface wave of dielectric waveguide. These peculiarities make difficulties in technical implementation and increase the cost of the device on the account of complex construction of the waveguide arrangement, higher precision requirements of the assembly, complexities of the alignment process of the elements.
The second disadvantage is the necessity of simultaneous rotation, in a single construction, not only the linear dielectric waveguide but also the cylindrical dielectric lens above the waveguide, which focuses downward radiation along the focal line coinciding with the axis of dielectric waveguide. Aperture angle of the antenna in the plane coinciding with the cross-section of the waveguide is established by the dimensions of the lens. At comparable measurements of the diffraction grating and the lens the latter, having finite focal distance, should be located on a significant distance from the dielectric waveguide. The higher is the size of receiver aperture and focal length, the higher will be this distance. This results in a potential increase of the dimensions of the antenna (its depth) and will not allow to implement the declared flat version of the antenna. With short focal lengths the curvature of the lens should be significant, which would result in increased width and mass and, correspondingly, would further increase the rotational momentum of inertia. These peculiarities complicate technical implementation of an antenna system with high operational parameters which, at the same time, should be easy to manufacture and have low cost.
The third disadvantage concerns limitations on the frequency bandwidth of radiation received by the radiometric system, it is known that the <<diffraction grating-dielectric waveguide>> electrodynamic system has expressed angle-frequency dependent properties, about 1° of shifting of the beam per 1% frequency change. During the reception of wideband radiation this results in the expansion of the beam width in the plane corresponding with the longitudinal axis of the waveguide and consequently in reduction of the efficiency of the system—deterioration of spatial resolution and quality of generated images, if the bandwidth of received frequencies is limited by installation of filters on the input of the receiver, this reduces radiometric sensitivity of the system and deteriorates the image quality because of reduced signal/nose ratio. Insufficient sensitivity of the radiometric receiver during singular beam high-speed scanning may lead to significant deterioration of overall image quality because of high noise factor in observation intervals of unitary picture elements. All these peculiarities are limiting the possibilities of implementation of an image generation system with high operational performance.
Fourth disadvantage of the mentioned systems and methods is because of high losses in the antenna and technical difficulties related to implementation of proposed types of diffraction gratings: multiple-sector, multiple-sector with alternating increment, spiral with alternating increment. Their fabrication at reasonable cost may only be possible based on the use of photolithographic methods while using substrates made of dielectric materials. In millimeter range the overwhelming majority of dielectric materials possess high imaginary components of dielectric permeability ∈″, which results in increase of losses in the antenna and reduction of radiometric sensitivity of the system or, if acceptable sensitivity is attained, ∈″ the system lacks required mechanical characteristics (either too brittle, or too flexible) and are too expensive when samples over ten centimeters in diameter with 1 mm thickness are needed. Among such materials are, particularly sapphire and silica glass. Significantly lower radiation losses can be obtained through the use of comb-shaped all-metal diffraction gratings, however fabrication of such gratings with variable curvature profile, or multiple sector gratings, with the required accuracy of profiles, is presently on the verge of possibility from the mechanical perspective. This makes the use of such gratings inefficient because of very high cost. Since active losses in the antenna define, to a significant extent, the overall noise temperature of the system and the attained sensitivity, the abovementioned peculiarities make the implementation of radiometric system of image generation with high technical specifications quite difficult.
At the same time, by utilizing the dispersion properties of such structures, through the use of corresponding procedures for processing of received noise signals, it appears possible to generate multiple-beam direction patterns of the antennas and to control the spatial orientation of these diagrams on the account of synchronous alteration of the parameters of the electrodynamic systems of antennas, providing a field of view in the sector of spatial angles. For example, such scheme of review may be implemented on the basis of reciprocal law of scanning with frame-based principle of image generation (Patent (UA) No 56347), (see
The antenna of such multiple beam scanning radiometer may be created on the basis of known engineering solutions, for example, Patent (UA) No 56347, and may contain a planar dielectric waveguide, disk-shaped diffraction grating placed under the dielectric waveguide mounted on the rotational output axis of electromechanical transmission, as well as a parabolic reflector, horn irradiator from planar dielectric waveguide to a hollow metallic waveguide and a disc position sensor, thereat the output of horn irradiator is the output of the antenna, and the input of electromechanical transmission and the output of disc position sensor are the control input and output of the antenna, respectively.
Among the advantages of the method disclosed in Patent UA No 56347 should be listed the possibility of generation of radio-thermal images with presence of only one ultra-high frequency input device in the system, thus significantly reducing its complexity and cost, in comparison with the version containing a beam-forming matrix. The second advantage of the prototype is M times reduction of the beam movement speed and √{square root over (M)} times improvement of the sensitivity of the system, in comparison with the singular beam scheme, on the account of concordant M times increase of the signal integration time.
In the same time the reciprocal principle of spatial observation by multiple beam direction pattern of the antenna, utilized in the prototype, has a disadvantage which is expressed in limited speed of image generation. This is related to the use of mechanical motion of disk-shaped diffraction grating with alternating direction in the process of controlling the spatial position of DPA, which takes place in a certain angular sector around the axes oriented near the working surface normal of the dielectric waveguide. For highly directional antennae the cross-dimensions of receiver aperture (diffraction grating) may reach tens of centimeters. Thereby moving elements of the antenna possess a quite high momentum of inertia and maximum attainable observation speeds and refreshing of images may not exceed several Hertz with reciprocal movement of beams. This is insufficient for the systems of operating supervision, where data refreshing speed should exceed 10 images per second.
The second disadvantage of this method is because of limitations of the attainable sector width of observation angles on that coordinate, by which frequency division of the reception directions is performed. The electrodynamic system of the antenna has angle-frequency dependence, which results in certain limitations of working bandwidth because of deteriorating of energy transformation coefficient on the brinks of the band at fixed parameters of the dielectric waveguide and diffraction grating. Thereat efficient transformation of volume electromagnetic waves into surface waves may take place in a limited bandwidth, around ˜16 to 20% from the central frequency. At realizable values of angle-frequency coefficient of the antenna about 0.9 to 1 degrees of the beam sweep per 1% frequency change the mentioned bandwidth determines the attainable size of the observation angle sectors by that coordinate with the value around 15° to 20°, which is insufficient for remote sensing and operating supervision of the environment.
Among disadvantages of the antenna in the prototype device is the need to change mutual positions of the diffraction grating and dielectric waveguide in the process of scanning. By turning the diffraction grating the orientation of scattering elements of the grating will change in relation to the phase front of electromagnetic wave propagating in the dielectric waveguide, on which account the parameters of mentioned electrodynamic system will change too, and, as a result, will change the spatial orientation of the antenna beam (beams). At the same time, such variation of the elements of electrodynamic system will also stipulate the change of energy characteristics of the antenna: transformation efficiency of volume electromagnetic wave into surface wave of dielectric waveguide declines with inclination of the beam (beams) from the initial position, at which scattering elements of the grating are oriented in parallel to the phase front of the surface wave of dielectric waveguide. Similarly, inclination of the beam from the initial position corresponding to the initial position of the grating brings to the increase of the width of the beam (beams) of the antenna as a result of effective dimensions of the receiver aperture in accordance with the change of aperture's projection on viewing direction; that is, inclination of the beam results in the reduction of antenna area utilization coefficient of the antenna. Thus, for the mentioned method of radiometric images generation energy-transfer factor of the antenna and beam width are functions of the scanning angle, which prohibits the attainment of equally high DPA parameters in the whole sector of observation angles, and therefore it is not possible to attain same image quality on the whole field; this potentially results in deterioration of quality of generated images.
Another disadvantage of the prototype antenna is related to technological complexities in the process of its fabrication and alignment. Since in the process of operation the diffraction grating and planar dielectric waveguide should be positioned on a certain calibrated distance, which is selected in the process of alignment of the antenna and should remain invariable in the process of scanning, construction of the antenna should satisfy these conditions. As a result, the requirements to mechanical characteristics of the elements—flat surface accuracy of the diffraction grating and planar waveguide, are quite high—which is a limiting factor for the types of applicable dielectric materials. For example, a planar waveguide made of polystyrene, which possesses quite high rigidity and stability of mechanical characteristics, is unsuitable in a millimeter range applications because of about twice higher losses in comparison with, for example, PTFE; PTFE, however, cannot be used without reservations in such construction because of its cold flow and instability of mechanical characteristics at exploitation period. Since rotation of the diffraction grating respective to dielectric waveguide is one of the key features of the mentioned method of image generation and thus defines the construction and mechanical characteristics for the material of dielectric waveguide, the mentioned features are among disadvantages of the antenna, reducing its attainable technical parameters, increasing its complexity and cost.
The essence of the first invention of the group is to improve the method of radiometric images generation on the account of transition from group reciprocal linear movement to isochronous circular movement of multiple-beam direction patterns of the antenna, thus-providing an improvement, of maximum speed of image generation, improvement of radiometric resolution in central part of the image and expansion of the sector of observation angles.
The essence of the second invention of the group is to improve the scanning multiple-beam antenna on the account of transition to circular principle of scanning, thus providing an increase of scanning speed, reduction of active losses, improvement of aperture area utilization coefficient, attainment of better technological effectiveness and reduction of manufacturing costs.
The first issue is resolved on account of the fact that, in the method of radiometric images generation, based on cyclical repeating of an algorithm, consisted of the procedures of measurement and processing of data, executed with the use of four basic time intervals, named as the calibration phase by first standard with Δtcs1 duration, calibration phase by second standard with Δtcs2 duration, external radiation reception phase with Δtex duration, and data processing phase with Δtpr duration, at that, data processing phase Δttr follows after the external radiation reception phase Δtex, and calibration phases Δtcs1 and Δtcs2 which may be executed in any order, precede the external radiation reception phase Δtex, at that, reception of external radio-thermal radiation takes place during the external radiation reception phase Δtex from a two-dimensional sector of angles represented in an orthogonal coordinate basis and characterized by independent coordinates Θ and Φ, calculated from a spatial vector defining the antenna aperture plane and by angular sector ΔΘ=(Θfin−Θini) of the Θ coordinate, with coordinates of the initial and final observation angles Θini and Θfin, respectively, as well as M (M≧1) independent observation directions with spatial orientation θm (M≧m≧1) along mentioned spatial Θ coordinate. M values of the radio-thermal radiation intensity Ei,m, simultaneously received by M beams of the antenna. These M values are processed in M reception channels concurrently and in accordance with a unified measurement procedure and are then transformed into a one-dimensional array of digital values [Cm] during the calibration phase by first calibration standard Δtcs1 simultaneously M reception channels receive the first calibration radiation with known or calculated intensity Tc1,m in units of temperature scale, and the received signals are processed concurrently and in accordance with a unified measurement procedure in M reception channels and are transformed into a one-dimensional array of digital values [Cc1,m] with dimensionality [M], during the calibration phase by second calibration standard Δtcs2 simultaneously M reception channels receive the second calibration radiation with known or calculated intensity Tc2,m in temperature scale units, and received signals concurrently and in accordance with unified measurement procedure are processed in M reception channels and transformed into a one-dimensional array of digital values [Cc2,m] with number of dimensions [M], during the processing phase Δtpr the received arrays of digital data [Cm], [Cc1,m], [Cc2,m], [Tc1,m], [Tc2,m] are processed simultaneously in accordance with the data processing procedure for calculation of radio-brightness temperatures of received radiation, as a result of which is formed a one-dimensional array of values with number of dimensions [M], the values [Tb,m] of which, represented in units of the temperature scale characterize distribution of intensity of radio-thermal radiation Ei,m,n for one independent direction of observation n (N≧n≧1) from N (N≧1) observation directions along a different from Θ direction independent spatial coordinate, at that, in addition to the above, θm directions simultaneously arise in a dispersive antenna with of radiometric system on the account of frequency division of reception directions on spatial coordinate Θ on M independent directions by splitting the general bandwidth of the radiometric system Δf into M narrower bandwidths Δfm, each of which characterizes a separate receiving channel number m with total number of these channels M, at that the procedure of measurement in each of M receiving channels includes consecutive operations of filtration and amplification of signals in ultra-high frequency range in general for ail channels bandwidth Δf=(fini−ffin), where fini and ffin, are, respectively, the initial and final values of radiation frequency received by radiometric system in ultra-high frequency (UHF) range, segregation of the signal in frequency band Δfm=(fm,ini−fm,fin), where fm,ini and fm,fin, respectively, are the initial and final values of frequency of received radiation in channel with number m attributed to the range of ultra-high frequencies, at that the mentioned values fm,ini and fm,fin successively change from channel to channel and are selected so that, along with bands Δfm in M reception channels without omissions covers the whole frequency band Δf, and θm directions corresponding to bands Δfm concordantly and without omissions cover the whole sector of angles ΔΘ, and, finally, successively executed in each channel operations of square-law detection, integration, analog-digital conversion and digital accumulation and besides, the procedure of data processing includes consecutively executed operations of calculating for each of m reception channels the Sm=(Tc1,m−Tc2,m)/(Cc1,m−Cc2,m) coefficients, defining the values of steepness of linear dependence of transformation of output digital values Cm into the values of external radiation radio-brightness temperatures Tb,m, and then calculations of Tb,m values according to found linear dependences proportionally as Tb,m=Sm·(Cm−Cc2,m)+Tc2,m with a following formation of a two-dimensional array [Tb,m,n] with number of dimensions [dimensionality] [M×N] for M·N independent observation directions by both independent coordinates of the image, in accordance with the invention formation of images takes place with simultaneous isochronous circular movement of M beams of the antenna and is implemented on the account of turning the receiver aperture of the antenna around a spatial axis defining the main observation direction with coordinates [Θmain, Φmain] during the revolution period Trev by angle Ψ=360° with simultaneous synchronous revolution of mentioned coordinate system around same spatial axis to the same angle Ψ=360° with simultaneous representation of image coordinates in coordinate system (Θ, Ψ) and introduction of file initial Ψini and final Ψfin values of observation angles by Ψ coordinate, defining the sector of observation angles ΔΨ=(Ψfin−Ψini) by Ψ coordinate while splitting this sector into N (N≧1) independent observation positions Ψn (N≧n≧1) along Ψ coordinate and introduction of the fifth basic time interval into the algorithm which is a part of the data processing procedure and named coordinate transformation phase with the duration Δtctr during which the procedure of transformation of spatial coordinates of the picture elements from coordinate system (Θ,Ψ) into reference frame (Θ,Φ) is performed for the generated two-dimensional array of values of radio-brightness temperatures [Tb,m,n], at that the main observation direction Θmain by coordinate Θ takes any values in the sector of angles from 0° to 90°, and by coordinate Φ the main observation direction Θmain takes zero value (Φmain=0), besides, certain phases can be executed multiple times in various combinations depending on the selected duration of execution of calibration phases by the first calibration standard Δtcs1, calibration by the second calibration standard Δtcs2, reception of external radiation Δtex in reference to revolution period Trev, specifically, reception phase of external radiation Δtex can be executed P times consecutively (P≧1), thus forming an accumulation cycle with duration Δtac, when P=1 the algorithm contains a group of consecutively executed calibration phase by first calibration standard Δtcs1, calibration phase by second calibration standard Δtcs2, reception phase of external radiation Δtex and processing phase Δtpr, repeating the mentioned group I consecutive times (I≧1), after which the coordinate transformation phase Δttr is executed, and when P>1 the algorithm consists of consecutively executed calibration phase by the first calibration standard Δtcs1 and calibration phase by the second calibration standard Δtcs2, after which repeatedly J times consecutively (J≧1) the group consisting of consecutively executed accumulation cycle Δtac, processing phase Δtpr and coordinate transformation phase Δttr, is executed, besides, data accumulation takes place with accumulation interval τm≦Δtex/N during the reception phase of external radiation Δtex with concordant increase of the accumulation interval τm in accordance with proximity of spatial coordinates θm to the main observation direction [Θmain], with accumulation interval τc1m≦Δtcs1 during the calibration phase Δtcs1 by first calibration standard and with accumulation interval τc2m≦Δtcs2 during calibration phase Δtcs2 by second calibration standard.
Such modification of the method of radiometric images generation allows to improve the speed of image generation, increase radiometric resolution in central part of the images, located near the main observation direction, extend the sector of observation angles while maintaining the number of processing channels M and frequency band Δf on the account of meeting the following conditions.
The second stated problem is resolved by the provision of an antenna containing a planar dielectric waveguide and a two-dimensional diffraction grating, irradiator, electromechanical transmission and a position sensor. The planar dielectric waveguide and the two-dimensional diffraction grating are associated by a diffraction field. The receiving aperture plane is positioned closest to the received radiation side of planar dielectric waveguide. The input of the irradiator is connected to the output of planar dielectric waveguide. The input of electromechanical transmission and output of the position pickup sensor are, respectively, the control input and control output of the antenna, in addition a pedestal unit, rotating waveguide transition and a rotating force canceller has been added. The electromechanical transmission, rotating force canceller, position sensor and rotating waveguide transition are mounted on the pedestal unit. The output shaft of electromechanical transmission, the rotating force canceller and the rotating waveguide transition are coaxial with the possibility of rotation around the common axis. The rotating force canceller, through a kinematic scheme, is linked to the output shaft of electromechanical transmission. The planar dielectric waveguide, two-dimensional diffraction grating and irradiator are mechanically rigidly bound with each other and form an integrated constructional assembly; which is named antenna rotor. The antenna rotor is mechanically rigidly bound with the output shaft of electromechanical transmission. The output of the irradiator is connected to the rotating input of the rotating waveguide transition, the immobile output of which is the output of the antenna.
This engineering solution allows an improvement in the speed of image generation, an increase in the radiometric resolution in central part of the images in the vicinity of the main observation direction, an increase in the scanning velocity, aperture area utilization ratio and ease of manufacture, and an expansion in the sector of observation angles without changing the number of processing channels M and invariable frequency band Δf. This solution is realized through the following criteria;
According to the present invention there is provided a method of radiometric image generation using a series of isochronous revolutions of a multi-beam antenna with a dispersion characteristic, wherein the antenna is combined with a multi-channel receiver with frequency channel separation to form an imaging unit, the method comprising cyclically executing the following phases: two separate calibration phases Δtcs1, Δtcs2 using first and second standards; external radiation reception phased Δtex, data processing phase Δtpr, and data transformation phase Δttr. During each revolution of the antenna, one or two full images are generated using this method. The reception phase of the external radiation Δtex may be executed consecutively P (P≧1) times forming an accumulation cycle Δtac with a duration P·Δtex. The image is typically a segment of a circle.
The total duration of the calibration phase by the first calibration standard Δtcs1, the calibration phase by the second calibration standard Δtcs2, the accumulation cycle Δtac, processing phase Δtpr and coordinate transformation phase Δttr, executed consecutively may be equal to the rotation time period Trev of the antenna.
Alternatively, the total duration of the calibration phase by the first calibration standard Δtcs1, the calibration phase by the second calibration standard Δtcs2, the accumulation cycle Δtac executed consecutively may be equal to the rotation time period Trev of the antenna. Alternatively, the consecutively executed calibration phase by the first calibration standard Δtcs1, calibration phase by the second calibration standard Δtcs2, reception phase of external radiation Δtex (P=1) and processing phase Δtpr may be performed cyclically N times in a row (I=N, where N is number of independent beam positions per revolution), with a total duration of the mentioned cycle of N repetitions equal to the rotation time period Trev. In this case, the coordinate transformation phase Δttr, is subsequently executed independently. The transformation phase Δttr is preferable performed during the revolution following the revolution during which the data was received.
Alternatively, the total duration of the execution of calibration phases by the first calibration standard Δtcs1, by the second calibration standard Δtcs2 and reception of external radiation Δtex is the same for any element of the cycle with a number i (I≧i≧1) and is equal to the (1/N)th part of the rotation period Trev, and the processing phase Δtpr may be executed independently in the course of regular (i+1)th element of the cycle.
In the course of execution of each regular element of the cycle with a number i (I≧i≧1) each of the calibration phases may foe alternately excluded, and in the course of execution of processing phase Δtpr the data is obtained for the (i−1) element of the cycle. In particular, in the course of execution of each regular element of the cycle with a number i (I≧i≧1) one of the two mentioned calibration phases is alternately excluded, either the calibration standard Δtcs1, or Δtcs2. In case of exclusion in the element of the cycle under number i, the calibration phases by the first calibration standard Δtcs1, in the course of execution of processing phase Δtpr the mentioned data arrays of values obtained are used for the (i−1)th element of the cycle in the capacity of data arrays of values [Cc1,m], [Tc1,m], where [Cc1,m], are digital outputs of M (M≧1) radiometric channels (1≦m≦M) in the case of receiving the signals from the first calibration standard, [Tc1,m] are calibration signals intensity for the first calibration standard with units of temperature. In the case of exclusion in the element of the cycle under the number i the calibration phases by the second calibration standard Δtcs2, in the course of execution of processing phase Δtpr the mentioned data arrays are used in the capacity of the data arrays of the values [Cc2,m], [Tc2,m], which are obtained for the (i−1) element of the cycle, where [Cc2,m], are digital outputs of M radiometric channels in the case of receiving the signals from the second calibration standard, [Tc2,m] are calibration signals intensity for the second calibration standard.
The total duration of the consecutively executed calibration phase by the first calibration standard Δtcs1 and the calibration phase by the second calibration standard Δtcs2, may be equal to rotation time period Trev and the consecutively executed accumulation cycle Δtac, processing phase Δtpr and coordinate transformation phase Δttr may be executed cyclically J times in a row (J≧1). In addition the data processing phase Δtpr and coordinate transformation phase Δttr may have a total duration which is less than rotation time period Trev and may be executed independently from the calibration phases Δtcs1, Δtcs2 and accumulation cycle Δtac within the time limits of the next rotation time period Trev.
The values of [Cc1,m], [Tc1,m], and [Cc2,m] [Tc2,m] data array elements for the current element of the cycle under number i (I≧i≧1) may be the mean arithmetic values for each element of these data arrays, obtained by utilization of K (K≧1) preceding significant of these elements in K preceding elements of the cycle, counted out from number i.
The capacity of expansion measure for accumulation cycle τm within the time period of external radiation reception Δtex, in accordance with the proximity of spatial coordinates θm to the main direction of observation Θmain, the following expression may be used
The main direction of observation Θmain may take one of the two values by Θ coordinate, respectively either Θini or Θfin, at that the spatial orientation of the aperture plane of the antenna remains unchanged in time.
The main direction of observation Θmain may alternatively take any value of the Θ coordinate, which are within the sector ΔΘ, with the exception of Θini, Θfin, at that the spatial orientation of the of the aperture plane of the antenna remains unchanged in time.
In either of the above configurations, the spatial orientation of the aperture, plane of the antenna is changed by an arbitrary law.
The main direction of observation Θmain may take value by Θ coordinate outside the ΔΘ sector, at that the spatial orientation of the aperture plane of the antenna remains unchanged in time, at simultaneous uniform linear movement of antenna in the same plane.
Furthermore, according to the present invention there is provided an antenna comprising an antenna rotor comprising a planar dielectric wave-guide, a two-dimensional diffraction grating and an irradiator and a rotating wave-guide transition configured to rotate relative to the antenna rotor. The planar dielectric wave-guide may be parallel to the diffraction grating. Alternatively or additionally, the planar dielectric wave-guide and the diffraction grating may be provided on a common substrate. In particular, the common substrate may be a dielectric material with a foil coating to provide the diffraction grating. The planar dielectric wave-guide may be non-parallel to the diffraction grating. This configuration provides a better electromagnetic field distribution across the diffraction grating as a result of a reduction in side lobes for this configuration. The largest gap is providing near the irradiator side.
The antenna may further comprise a force canceller configured to rotate relative to the antenna rotor. The antenna may further comprise an electromechanical transmission comprising a motor configured to rotate at least the antenna rotor around an axis in a first direction. The antenna may further comprise a second motor configured to rotate the force canceller in a second direction about the axis, opposite to the first direction. The antenna may further comprise a two-dimensional non-rotating axially symmetric dielectric lens. The lens axis may be coaxial with the axis of the electromechanical transmission.
The antenna may further comprise a sensor configured to measure the angular position of the antenna when if rotates. The sensor may be located within the electromechanical transmission.
The antenna according to the present invention may be combined with a multi-channel radiometric receiver with frequency channel separation in order to provide an imaging unit. The sensor may be further configured to synchronize the data processing means with the angular position of the antenna.
The imaging unit may further comprise, at least one radiation source for calibrating the multi-channel radiometric receiver. The radiation source is configured to provide two distinct reference signals. The first may be created with the active noise radiation source with attenuation of the signal by a directional coupler and the switch in “on” or “off” position. The second radiation reference signal may be the black body radiation of the device with the switch in the “off” position and active noise source in “off” position.
The imaging unit may further comprise a second radiation source for calibrating the multi-channel radiometric receiver. The imaging unit may further comprise means for processing data received by the multi-channel receiver and means for transforming the processed data.
The antenna or the imaging unit may be used to execute the above described method.
The present invention will now be described, by way of example only, with reference to the accompanying drawings in which:
Claimed method for generation of radiometric images is implemented in the following way (see,
An algorithm comprising of the procedures of measurement and processing of data, cyclically repeated in time and executed during five time intervals named as calibration phase by first standard with Δtcs1 duration, calibration phase by second standard with Δtcs2 duration, external radiation reception phase Δtex, which may be executed P times consecutively (P≧1), forming an accumulation cycle with Δtac duration, data processing phase with Δtpr duration, data transformation phase Δttr, at that successively executed data processing phase Δtpr and data transformation phase Δttr follow after the accumulation cycle Δtac of P repeated external radiation reception phases Δtex, and calibration phases Δtcs1 and Δtcs2 which are executed in any sequence, precede the accumulation cycle Δtac of P external radiation reception phases Δtex. At that, during any of the P external radiation reception phases Δtex external radio-thermal radiation is received from the environment from two-dimensional sector of angles, which is characterized by orientation of axes of spatial coordinates of the directional pattern of antenna in Θ and Ψ directions, with coordinates of initial observation angles, respectively, Θini and Ψini, final observation angles, respectively, Θfin and Ψfin, sector sizes, respectively, ΔΘ=(Θfin−Θini) and ΔΨ=(Ψfin−Ψini), and also M (M≧1) and N (N≧1) independent observation directions, respectively, along each of the mentioned spatial coordinates and with spatial orientation, respectively, θm(M≧m≧1) and ψn(N≧n≧1). For example, values of these parameters may be, by Θ coordinate; Θm=2°, Θfin=16° from the normal to the aperture plane of the antenna, ΔΘ=14°; by coordinate Ψ, Ψini=0°, Ψfin=+180° from horizontal, ΔΨ=180°, M=32, N=180, P=N=180.
Antenna of the radiometric system mechanically revolves around rotational axis, the position of which in respect to the normal to the aperture plane by Φ coordinate has zero deviation, but by Θ coordinate may take up any values in the sector of angles from 0° to 90°, for example, coinciding with the first beam of the direction pattern by Θ coordinate. Then rotation axis and main direction of observation, which define the center of the image, have the following coordinates; (Θmain=Θini=2°), (Θmain=0).
Directions of reception θm correspond to orientation of axes for each of m beams of the directional pattern of antenna and are generated simultaneously in an antenna with dispersive properties of the radiometric system on the account of frequency division receiving directions by the spatial coordinate Θ info M independent directions through division of the general bandwidth of the radiometric system Δf, which, for example, has the width Δf=14 GHz into M narrower frequency bands Δfm, which, for example, have the length Δfm=800 MHz, each of which characterizes a separate receiving channel number m with the overall number of these channels M. At that the bandwidths of adjacent channels are partially overlapping.
The procedure of measurement in each of M receiving channels is comprised of sequentially executed operations of filtering and amplification of signals in ultra-high frequency range in a general for ail receiving channels bandwidth Δf=(fini−ffin), where fini and ffin are, respectively, initial and final values of frequency of the radiation received by the radiometric system in ultra-high frequency range, for example, fini=86 GHz and ffin=100 GHz, signal extraction in frequency band Δfm=(Fm,ini−fm,fin), where fm,ini and fm,fin, respectively, are the initial and final values of frequency of the received radiation in the channel with number m associated to the range of ultra-high frequencies, at that, the mentioned values fm,ini and fm,fin are changing successively from channel to channel and are so selected that together, by Δfm bands in M receiving channels the whole frequency range Δf is covered without omissions, and by independent directions θm, corresponding to the Δfm bands, the whole sector of angles ΔΘ is covered consistently and without omissions. This is provided, because the width of any from the M beams in direction pattern of the antenna by coordinate Θ is approximately twice larger than the angular distance between adjacent directions, i.e. Δθ≈2(θm−θm+1), for example, Δθ=1° and neighboring beams are partially overlapping. At last, measurement procedure is completed by consecutively executed in each channel operations of square-law detection, integration with τm integration interval, analog-digital conversion and digital accumulation.
Temporal phase of reception of external radiation with Δtex duration, for example, Δtex=1 ms, is repeated P times in a sequence, for example, P=N, Δtac=180 ms, and during each element of this cycle 32-beam directional pattern of the antenna is oriented in a different from preceding direction ψn by coordinate Ψ, for example, from Ψini=0° to Ψfin=180° which defines propagation speed of the diagram ˜1°/ms, and corresponds to velocity of circular rotation of the antenna ˜2.8 revolutions/s and rotation period Trev=360 ms.
Received on each interval Δtex by M beams of the antenna M values of radio-thermal radiation intensity Ei,m, are processed in M receiving channels of the radiometric system concurrently and in accordance with the unified measurement procedure and transformed info a one-dimensional array of digital values [Cm], which is entered into the memory of radiometric system's computer. At that the integration intervals in measurement channels τm are selected in accordance with proximity of spatial coordinates θm to the main direction of observation. Since in this example we selected an orientation of the rotational axis of the antenna coinciding with spatial orientation of the first beam (Θmain=Θini), then for the last 32-nd beam the accumulation interval will remain τ32=Δtex=1 ms, for 16-th beam, because of two times reduction of radius (perimeter of a circle), it is selected twice longer, τ16=2·Δtex=2 ms, for 8-th beam, because of another twice reduction of the radius, it is selected 4 times longer, τ8=4·Δtex=4 ms, for the fourth, respectively, 8 times longer, for second—16 times longer, and for the first beam—32 times longer τ1=32·Δtex=32 ms. For intermediate numbers of beams that have not been mentioned here corresponding intermediate values of integration intervals are set, at that, the values of τm may, for example, be selected based on the following proportion:
Length of the accumulation cycle Δtac corresponds to rotation of the antenna by one-half turn, or by 180°, and obtained 180 one-dimensional arrays of values [Cm] are transformed info a two-dimensional array of values [Cm,n] with the number of dimensions [M, N]=[32, 180], which is entered into the memory of the computer of radiometric system.
Accumulation cycle Δtac, which is comprised of consecutively executed external radiation reception phases Δtex, is preceded by calibration phases by first and second calibration standards with duration Δtcs1 and Δtcs2, which are executed in any sequence, for example, Δtcs2=60 ms. Δtcs2=60 ms and initially is executed the calibration phase by first standard, then by the second. During the calibration phase by first standard direction pattern of the antenna is also moving by circular path, but the input waveguide of the radiometric receiver is disconnected from the antenna and connected to the output waveguide of the first calibrated standard. This operation may be executed, for example, with the use of controlled UHF switches. At that, M reception channels are simultaneously receiving the first calibration radiation with radiation intensities known for each channel Tc1,m in units of the temperature scale, and the received signals are processed in M receiving channels concurrently and in accordance with unified measurement procedure, and are transformed into a one-dimensional array of digital values [Cc1,m] with number of dimensions [M], which is entered into the memory of the computer of radiometric system. At that, integration intervals in measurement channels τm are selected in accordance with the duration of calibration phase τm≦Δtcs1.
Upon completion of the calibration phase by first calibrating standard, calibration phase by second calibration standard Δtcs2, is commenced, during which the direction pattern of the antenna also moves by circular path, however, input waveguide of radiometric receiver is disconnected from the first and connected to the output waveguide of the second calibration standard. This operation too is executed with the use of controlled UHF switches. Simultaneously M receiving channels are collecting the second calibration radiation with known intensity Tc2,m in temperature scale units, and received signals are processed concurrently and in accordance with unified measurement procedure in M receiving channels and transformed into a one-dimensional array of digital values [Cc2,m] with number of dimensions [M], which is entered into the memory of the computer of radiometric system. At that, accumulation intervals in measurement channels τm are selected in accordance with the duration of calibration phase τm≦Δtcs2.
Processing phase Δtpr is commenced upon the completion of accumulation cycle Δtac, for example, Δtpr=40 ms. During this phase the direction pattern of the antenna continues its movement by the circular path, input waveguide of radiometric receiver is disconnected from the second calibration standard and reconnected to the antenna, however the signals on the outputs of receiving channels aren't used. During the processing phase Δtpr arrays of digital data [Cm,n], [Cc1,m], [Cc2,m], [Tc1,m], [Tc2,m], which were entered into the memory of the computer, are concurrent processed in accordance with data processing procedure in order to obtain brightness temperatures of the received radiation, as a result of which is generated a two-dimension array of values with number of dimensions [M, N], the values [Tb,m,n] of which, represented in temperature scale units, characterize two-dimensional distribution of the intensity of radio-thermal radiation Ei,m,n which was received in the sector of spatial observation angles ΔΘ×ΔΨ. Procedure of data processing too is comprised of consecutively executed operations of calculating for each of the m channels the Sm=(Tc1,m−Tc2,m)/(Cc1,m−Cc2,m) values, which define the slope of linear dependence of transformation of output digital values Cm,n into the values of brightness temperatures of outer radiation Tb,m,n, calculation of values Tb,m,n according to found linear dependences in proportional denomination as Tb,m,n=Sm·(Cm,n−Cc2,m)+Tc2,m.
Upon completion of the processing phase Δtpr, during the coordinate transformation phase Δttr with duration of, for example, Δttr=20 ms, for two-dimensional array of brightness temperature values [Tb,m,n] it is executed the procedure of transformation of spatial coordinates of picture elements from the (Θ, Ψ) coordinate grid into the (Θ, Φ) coordinate grid, if needed, coordinate transformation phase may be supplemented by the procedure, of transformation of the coordinates of picture elements from (Θ, Φ) coordinate grid into a linear coordinate grid (X,Y). Mentioned transformations of coordinates may be executed on the basis of known trigonometric formulae (see, for example, Spravochnik po matematike dlya ingenerov i uchaschikhsya VTUZov. Bronshteyn I. N., Somendyayev K. A., M.:Nauka, 1981, 704 p.)
Thus, complete execution cycle of the algorithm in this example of implementation starts with calibration phase by first standard Δtcs1=60 ms, followed by calibration phase by second standard Δtcs2=60 ms, then follows accumulation cycle Δtac=180 ms consisting of 180 consecutively executed phases of reception of external radiation Δtex with duration of this phase equal to Δtex=1 ms, followed by the processing phase Δtpr=40 ms, then coordinate transformation phase Δttr=20 ms. Total duration of one cycle of execution of the measurement algorithm, accumulation, processing and data transformation is 360 ms and is equal to the duration of one revolution Trev the antenna around its rotational axis. With that, direction pattern of the antenna makes a full revolution and returns to its initial position with the value of coordinate Ψini=0°, and radiometric system generates an image which may be used for operative remotely sensed observations.
The mentioned algorithm may be repeated multiple times with continuous revolution of the antenna around its axes, as a result of which will be obtained a series of consecutive radiometric images. During temporal measurement of spatial orientation of the main direction of observation 4 on the account of auxiliary rotation of the whole antenna with the help of mechanical positioning devices, the images will be reflecting the changing observation conditions, at that, any part of the surrounding space may be consecutively observed.
In the considered example of implementation of the method for generation of radiometric images the algorithm is executed during one full revolution of the antenna around its rotational axis. At that, in the mentioned example the radiometric image is generated for half of the possible sector of observation angles by coordinate Ψ.
Other implementations are possible without affecting generality of claimed method, depending on selected duration of execution of calibration phases by first calibration standard Δtcs1, calibration by second calibration standard Δtcs2, reception of external radiation Δtex in reference to period of revolution Trev.
One alternate implementation of the method may be a combined operating sequence (see
Another alternate implementation of the method may be a combined operating sequence (see
Taking into account small volatility of calibration levels in close measurement time intervals, instead of mentioned arrays for the current element of the cycle with number i (I≧i≧1) may also be used arithmetic mean values for each element of the above mentioned arrays, obtained by using K (K≧1), for example, K=8, significant previous values of these elements in K previous elements of the cycle, starting from number i. In this case, on the account of additional averaging of data [Cc1,m], [Cc2,m], accuracy of determining radiation levels from calibration standards is improved.
Yet another alternative implementation of the method may be a combined operating sequence (see
On the assumption of anomalous multiplication of the internal noises of radiometric system on frequencies below 0.5+1 Hz, calibration of radiometric system should be executed no not more often than once in a second (Hersman M. S., Poe G. A. Sensitivity of total power radiometer with periodical absolute calibration//IEEE Trans, on Microwave Theory and Tech. Vol. 29, No. 1, pp. 32-40, 1981), which, considering the rather high rotational speed of the antenna, for example, 5 rev/s (or 10 rev/s) will result in insignificant short intermissions in the process of image generation, with respective durations of 200 ms, (or 100 mc). At that, each fifth (tenth) image in the continuous series of generated images will be missing, and during a corresponding time interval the preceding fourth (ninth) image may be reproduced one more time, which will not affect significantly on the efficiency of image generation process and data analysis.
In considered examples of implementation of the method the main direction of observation Θmain coincides with one of the outer beams of the antenna in the sector ΔΘ. Without transgression of generality we may also consider alternate implementations when the main direction of observation Θmain by coordinate Θ takes up any values in the sector of angles from 0° to 90°. In the case, when main direction of observation Θmain is inside the sector ΔΘ, there appear two groups of beams revolving with equal velocities, which are situated along common moving line but are generating images of different diameters. During transposition of these images and element averaging radiometric resolution in the central part of the image may be additionally improved on the account of constriction of the sector of observation angles. If Θmain is positioned in the middle of the sector ΔΘ, the diameters of these images will coincide. Then, on the account of 2 times constriction of the sector of observation angles either the frequency of image generation may be doubled, for the selected period of revolution Trev, or, with the same frequency of image, generation, on the account of their paired averaging, the equivalent integration interval may be doubled τme=2τm.
If the main direction of observation Θmain by coordinate Θ takes up a value situated outside the sector of angles ΔΘ, than inside the generated images appears an empty area, which may be filled up during linear motion of the antenna with a coordinated velocity, in this, case an alternate version of image generation with multiple-beam conical scanning may be implemented, for example, while mapping the surface from the board of a flight vehicle (see
As a device which would implement all the procedures of measuring, accumulating and processing the data, executed in the above mentioned sequence during the mentioned phases of execution Δtcs1, Δtcs2, Δtac, Δtpr and Δttr, may be used the known multiple-beam scanning radiometer (Patent UA 56347) which possesses a full-featured set of required functions, set of required elements and a corresponding structure of internal communications. At that, the antenna from the second invention from the group in present claim is used as the antenna for this radiometer.
The antenna contains (see
In order to create a multiple-beam direction pattern 11 in the mentioned antenna, it, as a constituent part of the scanning antenna, is used as a part of known multiple-beam UHF-radiometer (exemplified in Patent (UA) No 56347), providing band splitting of Δf frequencies into M frequency bands Δfm for the radio-thermal radiation received by the scanning antenna, at that by its output, controllable inputs and the output the scanning antenna should be connected to the input, controllable output and input of corresponding elements of the mentioned multiple-beam scanning UHF-radiometer. All comprising elements of the mentioned multiple-beam scanning UHF-radiometer with mentioned internal connections, except for scanning antenna, are shown on
As the pedestal unit 1 may be used any stationary base which has an alignment plane for the attachment of comprising elements of scanning antenna and providing an unfaltering space orientation of the main rotational axis 4 and electromechanical transmission 2 during the process of operation. As the pedestal unit 1 can also be used any supporting and turning arrangement possessing an alignment plane for the attachment of comprising elements of scanning antenna and providing, in the process of operation, operator-controlled manual or automatic, executed based on the operator's commands, correction of spatial orientation of its alignment pane. For example, in place of such pedestal unit can be used a tripod used by television operators for installation and control of the position of professional video cameras, for example, a tripod with manual control.
As the electromechanical transmission 2 may be used any mechanical transmission with hollow shaft 2-2, which can provide direct, or reduced synchronized isochronous revolution of the shaft and connected to the shaft elements with a given speed. At that, the input of the control line of the transmission is controllable input of the electromechanical transmission 2. For example, Patent (UA) No 56347 discloses an electromechanical transmission that may be realized en the basis of reduced stepper-motor. In this case it consists of a mechanically linked stepper motor and reducing gear, as well as pulsed amplifiers for the stepper motor control signals, with their number corresponding to the number of phase coils of the stepper motor, at that, each of the pulsed amplifiers is series-connected between the corresponding line of the input bus of the transmission 2 and the appropriate connector of the phase coil of the stepper motor. At that, inputs of the driver amplifiers and output shaft of the reducing gear are, respectively, the input of the control bus and shaft of the electromechanical transmission 2.
As bracing elements 3 may be used any known elements, for example, thread connection elements.
As revolving waveguide transition 5 may be used any known type of rotating waveguide linkage joint that will provide transmission of electromagnetic energy from its rotating waveguide input into its stationary waveguide output with small losses in the working bandwidth Δf of scanning antenna. For example, in place of rotating waveguide transition may be used the rotating waveguide linkage joint described in (Buduris J., Chenevie P. Ultra-high frequency chains (Theory and application). Translation from French./Editor A. L. Zinovieva.—M.:Sov. Radio, 1979,-288 p., pp. 130) and comprising an input and output sections of hollow rectangular waveguides, each of which has on its wide wall transition elements to a circular waveguide with transformation of the main wave H01 in the rectangular waveguide into the E01 wave of the circular waveguide. At that, the mentioned sections of circular waveguides are situated axially with the rotation axis and form a waveguide line with a rotary joint and a circular gap on the wall of the circular waveguide; electrical interlocking for ultra-high frequency currents is provided with the help of quarter-wave traps in the area of rotary joint. When using this type of waveguide joint in place of rotating waveguide transition 5, its transmission link based on circular waveguide with rotary joint installed inside of the hollow output shaft 2-2 of the electromechanical transmission 2, axially with the main rotational axis 4, one of the sections of rectangular waveguide are rigidly connected to the shaft 2-2, its waveguide flange is the waveguide input of the moving rotor section 5-2 of the transition 5, and second section of the rectangular waveguide is rigidly fixed on the basis 1, its waveguide flange is the waveguide output of the stator section 5-1 of the transition 5.
Canceller of angular momentum 6 is designated for compensation of angular momentum of the antenna rotor in the process of high-speed revolution, which makes difficult to change the spatial position of the main axis 4 because of gyroscopic action. An example of the structure of a canceller of angular momentum 8 is shown in
Planar dielectric waveguide 7 and diffraction grating 8 may be accomplished in accordance with known engineering solutions (see, for example, Skaniruyuschaya antenna samoletnogo radiometricheskogo kompleksa/Andrenko S. D., Evdokimov A. P., Kryzhanovskiy V. V., Provalov S. A., Sidorenko Yu. B.//Radiofizicheskiye metody I sredstva dlya issledovanlyaokruzhayuschey sredy v millimetrovom diapazone.: Sb.nauch, tr.—Kiev: Nauk, dumka, 1988.—s. 154-160). For example, planar dielectric waveguide 7 may be fabricated from a polystyrene sheet of given thickness with the use of mechanical plane grinding technology. Diffraction grating 8 may be accomplished as a flat metallic comb with lateral dimensions defined in an orthogonal coordinate base X and Y; the grating has a periodic structure by X coordinate and a flat structure by the Y coordinate. At that, coordinate plane Θ of the directional pattern of antenna coincides with the coordinate axis X and is orthogonal to coordinate axis Y. Dielectric waveguide 7 is located on some distance Δ from the periodic structure of the diffraction grating 8 and is linked to it by diffraction field. In order to create the given amplitude-phase distribution of the field by X coordinate the distance between the grating and the waveguide is selected during the alignment process and may change slightly by X coordinate.
Irradiator 9 may be accomplished in accordance with any known engineering solution for the exciter of planar dielectric waveguide providing a given transverse field structure at the interface with dielectric waveguide of selected aperture and concentration of electromagnetic energy on the output flange of the irradiator 9 with the structure of field for the main wave H01 of the standard hollow metallic waveguide. In place of irradiator 9 may be used a horn feeder or horn-parabolic exciter (see, for example, Skaniruyuschaya antenna samoletnogo radiometricheskogo kompleksa/Andrenko S. D., Evdokimov A. P., Kryzhanovskiy V. V., Provalov S. A., Sidorenko Yu. B.//Radiofizicheskiye melody I sredstva dlya issledovaniyaokruzhayuschey sredy v millimetrovom diapazone.: Sb.nauch, tr.—Kiev: Nauk, dumka, 1988.—s. 154-160), providing a single transmitting mode of electromagnetic energy. An additional design requirement to irradiator 9 in this antenna is the need of consecutive turning of the wave propagation direction by 90°, two times, which simplifies the placement of output flange of the irradiator 9 on the back side of the diffraction grating 8 near rotational axis 4, providing the size of the antenna rotor in the rotation plane to be maximally close to the aperture of diffraction grating 8, thus reducing the size of the antenna rotor.
Position sensor 10 may be accomplished on the basis of any engineering solutions providing generation of pulsed electric signal while given spatial position of the controlled object is attained, for example, based on a magnetic sensor. At that, on one of the construction elements of the antenna rotor, for example, on the back side of the diffraction grating 8 is placed a permanent magnet, and on the pedestal unit 1 near the circular path of rotation of the magnet is positioned an inductive coil, which is part of the oscillating circuit of an electronic generator. During the passage of the magnet the frequency of the generator changes, thus operating the comparator, which generates the output signal of the position sensor 10.
Parameter values during consideration of the antenna system were used the abovementioned values of these parameters on the example of implementation of the method for generation of radiometric images by first invention.
The antenna operates in the following way (see
Receiver 12 provides band splitting of frequencies Δf of the received radio-thermal radiation into M frequency hands Δfm. On the account of expressed dispersion properties of mentioned open electrodynamic system of the antenna, in each of M received frequency bands Δfm in the sector of angles ΔΘ×ΔΦ transformation of the falling radio-thermal radiation is accomplished with varying efficiency. As a result, at each given moment of time the antenna by angular coordinate Θ, calculated from
As a result of rotation of the antenna rotor, the M-beam direction pattern also rotates synchronously, and each of 11-m beams is moving by its cone-shaped moving line depending on deviation θm of the particular beam 11-m from the selected main direction of observation Θmain in the plain of values Θ. For example, initial orientation of the aperture plane of the antenna and main rotational axis 4 may be selected in such a way that one of the outer beams in M-beam direction pattern would coincide in direction with the axis 4. While turning the M-beam direction pattern in full rotation angle Ψ equal to 360°, the antenna has full view of cone-shaped sector of spatial angles, which has, in place of its spatial axis, the main rotational axis 4 and the aperture at the vertex of a cone is 2ΔΘ.
In the process of scanning angular momentum of the antenna rotor is fully cancelled on the account of turning in the opposite direction and with required speed the angular momentum canceller 6. At that, spatial orientation of the sector of observation angles of the antenna can be changed without any significant effort by means of changing the spatial orientation of the alignment plane of the pedestal unit 1.
Independent angular positions of the antenna rotor in time are rigidly linked with the structure of controlling signal entering the electromechanical transmission 2 from radiometric receiver 12. As a result, it is provided synchronization of data in receiver 12 and mutual spatial binding of responses of receiver 12 to the received radio-thermal radiation to current spatial positions of the M-beam direction pattern.
With each full revolution of the antenna rotor position sensor 10 generates a pulsed signal, which enters the radiometric receiver 12. On the account of this is provided the initial temporal synchronization of signals in radiometric receiver 12, and on its output it generates an array of output values of brightness temperatures, which represents the intensify distribution of radio-thermal radiation in spatial sector of observation angles in temperature scale units. At that, the image may be generated both in an angular coordinate system 13, associated with the rotational axis 4, and in an rectangular coordinate system 14, associated with external, in respect to the antenna, reference system.
In the example shown in
In the example shown in
In the example shown in
In the example shown in
The example shown in
In addition to the functionality of the imaging unit as described above, the device 100 includes a video camera 118, illumination 120, a GSM antenna 122 and a flash memory and removable memory card 124. The illumination 120 takes the form of a plurality of LEDs spaced around the periphery of the lens 102. The data from the video camera 118 and the GSM antenna 122 is processed by suitable video and GSM link electronics 126. The image data arising from the processed antenna data, together with the data from the video camera 118 can be stored in the memory and/or on the card 124 or transferred using a GSM link to a remote location for storage or further processing. Control of the device 100, including control of the transfer of data and combined real time optic/radiometric images is executed using a touch screen 128 in combination with a headset and microphone 129. The touch screen 128 is configured so that it is visible to the user when holding the device 100. The headset and microphone 129 are connected info the device 100, either physically or via a Blue tooth or similar wireless protocol. The memory card 124 is conveniently located within the handle 103 which can be provided with an access port (not shown) to allow the memory card 124 to be changed.
The power for the device 100 may be incorporated into the device housing. However, batteries can add considerably to the weight of the device and therefore, for ease of use the batteries may be provided in a separate pack 130 which the user may wear around the waist. The battery pack 130 will be attached to the device at a power plug 132.
The invention is not limited for use at the hand-held scale. Indeed, with an increase in aperture size and an increase in range a similar device could be used for covert defection or to aid landing of helicopters.
The present application claims priority as a continuation application to a patent application entitled “Method For Formation of Radiometric Images And An Antenna For Implementation Of The Method”, U.S. patent application Ser. No. 14/457,974, filed Aug. 12, 2014, which is a Continuation of U.S. application Ser. No. 13/140,202, filed Aug. 25, 2011, now U.S. Pat. No. 8,836,598, Issued Sep. 16, 2014, which is a U.S. National Stage of PCT/GB2008/051218, filed Dec. 19, 2008, of which are herein incorporated by reference in their entirety.
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| 20150320322 A1 | Nov 2015 | US |
| Number | Date | Country | |
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| Parent | 14457974 | Aug 2014 | US |
| Child | 14802593 | US | |
| Parent | 13140202 | US | |
| Child | 14457974 | US |
