CN114047473B - Arrival angle and polarization angle measuring method based on polarization sensitive annular array - Google Patents

Arrival angle and polarization angle measuring method based on polarization sensitive annular array Download PDF

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CN114047473B
CN114047473B CN202111210703.3A CN202111210703A CN114047473B CN 114047473 B CN114047473 B CN 114047473B CN 202111210703 A CN202111210703 A CN 202111210703A CN 114047473 B CN114047473 B CN 114047473B
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沈志博
唐勇
刘俊
朱全江
王浩丞
王星斗
傅劲松
吕强
曲焕全
刘胜云
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CETC 29 Research Institute
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Abstract

The invention provides an arrival angle and polarization angle measuring method based on a polarization sensitive annular array, which is used for receiving data of a plurality of signals through the polarization sensitive annular array; constructing an orthogonal polarization redundant dictionary for each signal according to the spatial sparsity of the signal; sparse reconstruction is carried out on the signals through the obtained orthogonal polarization redundant dictionary to determine the two-dimensional arrival angle of the signals and the rough measurement value of the signal polarization angle; reconstructing an orthogonal polarization redundant dictionary according to the known two-dimensional arrival angle, and performing sparse reconstruction on the signals to obtain an accurate measurement value of the signal polarization angle; the method utilizes the polarization sensitive annular array, reduces the influence of antenna mismatch on the direction-finding performance, decomposes the signal multidimensional parameter joint measurement into independent processing of a frequency domain, a space domain and a polarization domain, and avoids the multidimensional joint search process, thereby greatly improving the parameter calculation efficiency and realizing the joint rapid measurement of angles and polarizations.

Description

Arrival angle and polarization angle measuring method based on polarization sensitive annular array
Technical Field
The invention relates to the field of array signal processing, in particular to an arrival angle and polarization angle measuring method based on a polarization sensitive annular array.
Background
The conventional direction-finding antenna array generally adopts a monopole array mode, as shown in fig. 1, and a plurality of single-polarized antenna units are annularly and uniformly arranged to form an array. The space electromagnetic signals possibly arrive at the antenna array in any polarization mode, the traditional monopole antenna uniform array mode has the problem of partial antenna unit polarization mismatch, the antenna unit mismatch gain loss is 20-25 dB, the effective antenna units of the antenna array are directly reduced, the direction finding error is increased, and the problems of high-frequency range direction finding is fuzzy, even direction finding cannot be achieved and the like are directly caused.
The existing array direction finding algorithm is mainly represented by a multiple signal classification (Multiple Signal Classification, MUSIC) method and a sparse reconstruction method.
For K far-field signals in space to be incident on the array, the array receiving data x (t) at the time t is:
Figure BDA0003308724830000011
in the formula
Figure BDA0003308724830000012
Represents the center frequency, pitch, azimuth angle of arrival, polarization amplitude angle and polarization phase angle, etc., of the kth signal, +.>
Figure BDA0003308724830000013
A steering vector representing the kth signal, s (t) being the signal vector, n (t) being the noise vector, A representing the array pattern, < >>
Figure BDA0003308724830000014
The prior MUSIC direction finding algorithm carries out eigenvalue decomposition on an array received data covariance matrix, utilizes orthogonality of a signal subspace and a noise subspace, obtains a space spectrum through multidimensional parameter joint search, and corresponds to a two-dimensional arrival angle and a polarization angle of a signal at the position of a maximum value of a spectrum peak, wherein a spectrum peak search calculation formula is as follows
Figure BDA0003308724830000015
The existing direction-finding method based on sparse reconstruction utilizes sparsity of signal incoming wave directions in a space domain to construct a multidimensional joint redundant dictionary, a sparse reconstruction model of signals is obtained, and a two-dimensional arrival angle of space signals is obtained by solving positions of non-zero coefficients in a sparse vector z (t), wherein the redundant dictionary and the sparse reconstruction model are shown in the formulas (3) - (4):
Figure BDA0003308724830000016
x(t)=Dz(t)+n(t) (4)
the existing MUSIC algorithm and sparse reconstruction algorithm both need to measure the two-dimensional arrival angle and polarization of the signal through a multi-dimensional search process (frequency domain, angle domain, polarization domain and the like), and the higher the required direction finding precision is, the wider the frequency band is, the denser the search grid division is, the larger the calculation amount of spectral peak search or sparse reconstruction solution is, the more obvious the parameter calculation efficiency is reduced, and the real-time processing requirement is difficult to meet.
Disclosure of Invention
Aiming at the problems that in the prior art, in the combined measurement of the two-dimensional arrival angle and polarization, the array unit antenna is mismatched, the operand is large, the direction finding real-time requirement is difficult to meet, and the like, the method for measuring the arrival angle and the polarization angle based on the polarization sensitive annular array is provided, and the combined measurement of the center frequency, the two-dimensional arrival angle and the polarization parameter can be obtained at the same time.
The technical scheme adopted by the invention is as follows: an arrival angle and polarization angle measuring method based on a polarization sensitive annular array comprises the following steps:
step 1, receiving data of a plurality of signals through a polarization sensitive annular array, carrying out Fourier transform on the received data to obtain a frequency domain model, and simultaneously measuring the frequency of each signal;
step 2, constructing an orthogonal polarization redundant dictionary for each signal according to the spatial sparsity of the signal;
step 3, performing sparse reconstruction on the corresponding signals on the orthogonal polarization redundant dictionary to obtain a space-polarization sparse representation model of the signals;
step 4, solving the space-polarization sparse representation model to obtain a sparse vector, and extracting non-zero elements in the sparse vector;
step 5, determining the two-dimensional arrival angle of the signal through the position of the non-zero element in the orthogonal polarization redundant dictionary; meanwhile, calculating a coarse measurement value of the signal polarization angle according to the polarization components of non-zero elements in the sparse vector;
and 6, repeating the steps 3-5 to obtain rough measurement values of the two-dimensional arrival angles and the polarization angles of all signals.
Further, in the step 2, the method for constructing the orthogonal polarization redundant dictionary includes:
based on the spatial sparsity of the signal, the frequency is f k The two-dimensional arrival angle of the signals is discretely divided, and the number of grids is N s Constructing orthogonal polarization redundant dictionary
Figure BDA0003308724830000021
Figure BDA0003308724830000022
wherein ,
Figure BDA0003308724830000023
consisting of the different polarization component responses of the array.
Further, in the step 3, a space-polarization sparse representation model of the signal:
Figure BDA0003308724830000024
wherein ,x(fk ) Is of frequency f k A space-polarization sparse representation model of the signal of (c),
Figure BDA0003308724830000025
for the sparse vector, n (f) represents the noise vector.
Further, the specific process of the step 4 is as follows: solving a space-polarization sparse representation model to obtain a sparse vector, solving non-zero elements, and converting the sparse vector into a convex optimization problem to solve in the solving process; the convex optimization problem is expressed as follows:
Figure BDA0003308724830000031
wherein z is a sparse vector, D is a redundant dictionary, x is a signal vector, and ε represents a reconstruction error.
Further, the method for calculating the coarse measurement value of the signal polarization angle in step 5 comprises the following steps:
Figure BDA0003308724830000032
Figure BDA0003308724830000033
wherein ,(γkk ) As the polarization angle of the signal,
Figure BDA0003308724830000034
the polarization components of the polarization angles of the signals in the h and v directions are respectively.
Furthermore, the method also comprises a high-precision signal polarization angle measurement method, wherein the polarization angle is uniformly and discretely divided on the known signal arrival angle, a new polarization redundancy dictionary is constructed, and the accurate measurement value of the signal polarization angle can be obtained by executing the steps 3-5 by adopting the new polarization redundancy dictionary.
Further, the new polarization redundancy dictionary is:
Figure BDA0003308724830000035
where γ represents the argument in polarization angle.
Compared with the prior art, the beneficial effects of adopting the technical scheme are as follows: the method provided by the invention can be used for simultaneously obtaining the measurement of the signal center frequency, the two-dimensional arrival angle and the polarization parameter. The method utilizes the polarization sensitive annular array, reduces the influence of antenna mismatch on the direction-finding performance, decomposes the signal multidimensional parameter joint measurement into independent processing of a frequency domain, a space domain and a polarization domain, and avoids the multidimensional joint search process, thereby greatly improving the parameter calculation efficiency and realizing the joint rapid measurement of angles and polarizations.
Drawings
FIG. 1 is a schematic diagram of a prior art single polarized annular array.
Fig. 2 is a flow chart of the angle and polarization angle measurement method according to the present invention.
Fig. 3 is a schematic view of a polarization-sensitive annular array according to the present invention.
FIG. 4 is a diagram showing the construction of a measuring apparatus according to an embodiment of the present invention.
FIG. 5 is a schematic diagram of two-dimensional angle of arrival measurement according to an embodiment of the present invention.
FIG. 6 is a diagram illustrating the measurement results of the polarization angle according to an embodiment of the present invention.
Fig. 7 is a schematic diagram showing the comparison of the measurement accuracy of the measurement scheme proposed by the present invention and the measurement accuracy of the angle of the single polarized annular array.
FIG. 8 is a schematic diagram showing the comparison of the calculation time of the measurement method and the multidimensional joint search method according to the present invention.
Detailed Description
The invention is further described below with reference to the accompanying drawings.
The invention solves the problems of mismatching of array unit antennas, large operand and the like in the joint measurement of the angle and the polarization of the array signals. Compared with the traditional angle and polarization combined measurement method, the scheme reduces the influence of antenna mismatch on the direction-finding performance, avoids the multidimensional combined search process, greatly reduces the operation amount, has higher calculation efficiency, and can improve the real-time direction-finding performance of the array signals. The specific scheme is as follows:
as shown in fig. 2, a method for measuring an arrival angle and a polarization angle based on a polarization sensitive annular array is provided, which comprises the following steps:
step 1, receiving data of a plurality of signals through a polarization sensitive annular array, and performing Fourier transform on the received data to obtain a frequency domain model
Figure BDA0003308724830000041
At the same time measuring the frequency of the signals +.>
Figure BDA0003308724830000042
Step 2, for a spatial frequency f k Based on spatial sparsity of signals, constructing an orthogonal polarization redundant dictionary for each signal
Figure BDA0003308724830000043
Step 3, in the orthogonal polarization redundant dictionary
Figure BDA0003308724830000044
Performing sparse reconstruction on the corresponding signals to obtain a space-polarization sparse representation model of the signals; />
Step 4, solving the space-polarization sparse representation model to obtain a sparse vector
Figure BDA0003308724830000045
Extracting non-zero elements in the sparse vector;
step 5, determining the two-dimensional arrival angle of the signal through the position of the non-zero element in the orthogonal polarization redundant dictionary; meanwhile, calculating a coarse measurement value of the signal polarization angle according to the polarization components of non-zero elements in the sparse vector;
and 6, repeating the steps 3-5 to obtain rough measurement values of the two-dimensional arrival angles and the polarization angles of all signals.
Considering K fully polarized far-field narrowband signals in space of interest to be incident on an antenna array, wherein the center frequency, angle of arrival, polarization angle of the kth (k=1, 2,..k) signal are f, respectively k
Figure BDA0003308724830000046
wherein θk
Figure BDA0003308724830000047
γ k E [0, pi/2) represents the polarization auxiliary angle, eta k E [ -pi, pi) represents the polarization phase difference, then the polarization sensitive annular array received data x (t) can be expressed as
Figure BDA0003308724830000048
Wherein A= [ a ] 1 ,a k ,...,a K ]For array flow pattern, s (t) = [ s ] 1 (t),s 2 (t),...,s K (t)]Is a signal vector s k (t) represents the kth signal, n (t) represents the mean value 0, and the variance is σ 2 Is a complex gaussian white noise of (c). a, a k Kronecker product of polarization-oriented vectors and spatial-oriented vectors, i.e.
Figure BDA0003308724830000051
in the formula ,
Figure BDA0003308724830000052
is a airspace guide vector,>
Figure BDA0003308724830000053
and steering vectors for the polarization domain. The center of the polarization sensitive annular array is used as a reference point (namely the origin of a coordinate system), and the number of the polarization sensitive annular array is +.>
Figure BDA0003308724830000054
Is the direction unit vector on the space rectangular coordinate system, l m For each element antenna position vector, the space phase shift factor of the incident signal to the array is
Figure BDA0003308724830000055
Then airspace guide vector +.>
Figure BDA0003308724830000056
Can be expressed as
Figure BDA0003308724830000057
For an orthogonal dual polarized element antenna, its polarization steering vector can be expressed as
Figure BDA0003308724830000058
Transforming the received data of the polarization sensitive annular array into a frequency domain to obtain a frequency domain model representation model as
Figure BDA0003308724830000059
After the signals are transformed into the frequency domain, the signals of all frequencies can be independently processed, so that the frequency domain joint search is avoided, and the processing dimension is reduced. The space electromagnetic signal can be incident on the antenna array in any polarization mode, the polarization sensitive annular array adopts orthogonal dual polarization sensitive array elements, so that the problem of polarization mismatch is effectively avoided, and the number of effective antennas of the array under any polarization incidence is ensured. The polarization sensitive annular array acquires polarization information of the space electromagnetic signals by utilizing each polarization sensitive array element, and acquires DOA information of the space electromagnetic signals by utilizing an array geometry structure to perform airspace sampling, so that joint measurement of signal angles and polarization angles is obtained.
According to the sparse reconstruction theory, an incident signal is sparse in a space domain, so that a sparse reconstruction model can be established in the space domain, the most direct method is to take a guide vector of any potential DOA and polarization angle of the signal as a column vector thereof to construct an angle-polarization multi-dimensional joint redundant dictionary, but the length of the multi-dimensional joint redundant dictionary is the product of the grid number of parameters of each dimension, the computation amount of sparse reconstruction is huge, and real-time calculation is difficult. Therefore, on the premise that signals can be sparsely represented, how to reduce the length of the redundant dictionary is particularly critical.
According to electromagnetic field theory, any polarized electromagnetic wave can be represented by a group of bases, i.e. any polarized electromagnetic wave can be decomposed into the following forms
e=he h +ve v (10)
in the formula eh and ev The unit polarization vectors of the directions are respectively, h and v are complex coefficients after polarization decomposition, and the polarization auxiliary angle and the phase angle of the signal can be expressed as
Figure BDA0003308724830000061
The polarization information characterizing the incident signal is responsive to different polarization components of the polarization sensitive annular array.
Based on the spatial sparsity of the signal, the frequency is f k The two-dimensional arrival angle of the signals is discretely divided, and the number of grids is N s Constructing orthogonal polarization redundant dictionary
Figure BDA0003308724830000062
As shown in (12)
Figure BDA0003308724830000063
in the formula
Figure BDA0003308724830000064
Is made up of the different polarization component responses of the array (any polarization can be synthesized). The constructed redundant dictionary is irrelevant to DOA, polarization mode and the like of an actual information source, and the polarization domain and the angle domain are independently processed. Multiple signals (i.e., co-frequency multiple signals) may exist at the same frequency, where all possible angle values are discretely divided, and a redundant dictionary is created to simultaneously estimate the angles of arrival of all signals at that frequency.
Sparse representation can be performed on signals by using redundant dictionaries to obtain the frequency f k An angle-polarization domain sparse representation model of the signal of (2) as shown in formula (13)
Figure BDA0003308724830000065
in the formula ,
Figure BDA0003308724830000066
for sparse vectors, ++>
Figure BDA0003308724830000067
In which there are only K non-zero coefficients and N s -K zeros (or approximately zero), the positions of the non-zero elements in the redundant dictionary corresponding to the actual directions of arrival of the K spatial signals, x (f) k ) Is of frequency f k A spatio-polar sparse representation model of the signal of +.>
Figure BDA0003308724830000068
For the sparse vector, n (f) represents the noise vector.
. Solving for sparse vectors
Figure BDA0003308724830000069
The two-dimensional arrival angle estimation of the corresponding signal can be obtained. According to the sparse reconstruction theory, the non-zero element solution can be converted into a convex optimization problem shown in equation (14).
Figure BDA00033087248300000610
Wherein z is a sparse vector, D is a redundant dictionary, x is a signal vector, and ε represents a reconstruction error.
Solving by a sparse reconstruction algorithm
Figure BDA00033087248300000611
After that, pass->
Figure BDA00033087248300000612
Middle NOTThe position of the zero element in the redundant dictionary is calculated to obtain the two-dimensional arrival angle of the signal; the redundant dictionary is a grid divided according to angles, so that positions and angle values of non-zero elements are in one-to-one correspondence, and corresponding angles are obtained by obtaining the positions of the non-zero elements. The polarization angle of the signal can be determined by the polarization component of the non-zero element +.>
Figure BDA00033087248300000613
and
Figure BDA00033087248300000614
The amplitude is calculated as shown in formula (15).
Figure BDA00033087248300000615
The result of the calculation using the formula (15) is a rough measurement of the polarization angle.
If it is necessary to obtain high-precision polarization angle measurement (mainly polarization auxiliary angle), the polarization angle can be uniformly and discretely divided on the known signal arrival angle, and the number of divided grids is N s And constructing a polarization redundancy dictionary as shown in a formula (16).
Figure BDA0003308724830000071
Gamma denotes the argument in polarization angle.
And (3) performing sparse reconstruction on the signals in a polarization domain by using the formula (16), so as to obtain accurate measurement of the polarization auxiliary angle.
In this embodiment, the arrival angle and polarization measurement of a plurality of radiation source signals are performed by performing a radiation source test in a microwave darkroom as shown in fig. 4, and it has been verified that the method proposed by the present invention has the following test conditions:
1) 4 radiation source antennas are erected in a microwave darkroom, a direction finding system is arranged on a turntable, and the angles of the radiation sources are
Figure BDA0003308724830000072
Are set to (-17 °,5 °), (-5 °, -10 °), (2 °,15 °), (15 °, -3 °) respectively. The polarization angle of the antenna of the radiation source 1 can be changed from 0-90 degrees by controlling the polarization synthesis source, the radiation source 2 is horizontally polarized, the radiation source 3 is vertically polarized, and the radiation source 4 is obliquely polarized by 45 degrees.
2) The radiation sources 1,2, 3, 4 are arranged to radiate analog pulse signals, and the signals overlap in the time domain
Specifically, the antenna array adopts a polarization sensitive annular array as shown in fig. 3, the unit antennas are orthogonal dual-polarized antennas, the phase centers are coincident, and M (m=8) unit antennas are arranged in an annular shape. The radio frequency signals received by the antenna array are subjected to down-conversion to intermediate frequency signals through a switch assembly, a frequency conversion assembly and the like, then the intermediate frequency signals are subjected to parallel sampling processing through a multichannel digital acquisition processor, and sampling data are transmitted to a signal processor for storage and processing.
And executing the measuring method on the sampling data to obtain a two-dimensional arrival angle, a polarization angle rough measuring value and a polarization angle accurate measuring value. As shown in fig. 5, the present invention enables accurate measurement of the two-dimensional angle of arrival of all 4 radiation sources. The results of fig. 6 show that the present invention can correctly measure the polarization angles of 4 radiation sources.
The method of the invention is compared with the traditional single-pole annular array method. Switching on the No. 2 and No. 3 radiation sources, controlling the output power of the signal source, so that the received signal-to-noise ratio (SNR) is changed from 0dB to 15dB, and respectively counting root mean square errors (counted according to the processing results of 1000 pulse data under each SNR) of two-dimensional angle measurement; as shown in FIG. 7, the method of the invention can accurately measure the two-dimensional arrival angles and polarization of a plurality of frequency signals in a wide frequency band, the maximum value of the root mean square error is not more than 0.5 DEG under the condition of high signal-to-noise ratio, and the maximum value of the root mean square error is not more than 0.2 DEG under the condition of low signal-to-noise ratio. In contrast, if the single-polarized annular array is adopted, the number of effective array elements is reduced and the angle measurement accuracy is obviously reduced due to antenna mismatch, so that the polarization-sensitive annular array mode of the method is proved to be obviously superior to the single-polarized annular array mode.
The method of the present invention is compared with a conventional multidimensional joint search method. The angle of the single-open No. 4 radiation source is-45 degrees, the polarization angle is 0-90 degrees, the stepping interval is adjusted, 2 degrees, 1.5 degrees, 1 degrees, 0.5 degrees, 0.3 degrees, 0.2 degrees and 0.1 degrees are respectively taken, and the angle and the polarization measurement time (according to the total time result statistics of continuous 100 times of angle and polarization measurement) of the multi-dimensional combined search method and the method are counted. As shown in FIG. 8, the invention adopts the independent processing mode of frequency domain, angle domain and polarization domain, improves the measurement efficiency, and basically keeps the operand unchanged under the condition of reducing the search interval of angle and polarization. In contrast, if the multidimensional joint search mode (for example, angle and polarization joint search) is directly adopted, the operand is obviously increased, and the requirement of real-time direction finding cannot be met. Therefore, the direction finding processing real-time performance of the method is proved to be obviously superior to that of a multidimensional joint search method.
The verification shows that the polarization sensitive annular array is adopted to reduce the influence of antenna mismatch on the direction finding performance, signals are decomposed into a frequency domain, an angle domain and a polarization domain for independent processing, a multidimensional joint search process is avoided, the operand is greatly reduced, and the high-precision real-time measurement of the two-dimensional arrival angle and the polarization angle can be realized.
The invention is not limited to the specific embodiments described above. The invention extends to any novel one, or any novel combination, of the features disclosed in this specification, as well as to any novel one, or any novel combination, of the steps of the method or process disclosed. It is intended that insubstantial changes or modifications from the invention as described herein be covered by the claims below, as viewed by a person skilled in the art, without departing from the true spirit of the invention.
All of the features disclosed in this specification, or all of the steps in a method or process disclosed, may be combined in any combination, except for mutually exclusive features and/or steps.
Any feature disclosed in this specification may be replaced by alternative features serving the same or equivalent purpose, unless expressly stated otherwise. That is, each feature is one example only of a generic series of equivalent or similar features, unless expressly stated otherwise.

Claims (7)

1. The arrival angle and polarization angle measuring method based on the polarization sensitive annular array is characterized by comprising the following steps of:
step 1, receiving data of a plurality of signals through a polarization sensitive annular array, carrying out Fourier transform on the received data to obtain a frequency domain model, and measuring the frequency of each signal according to the frequency model; the unit antennas of the polarization sensitive annular array are orthogonal dual-polarized antennas, the phase centers are coincident, and the unit antennas are arranged according to an annular shape;
step 2, constructing an orthogonal polarization redundant dictionary for each signal according to the spatial sparsity of the signal;
step 3, performing sparse reconstruction on the corresponding signals on the orthogonal polarization redundant dictionary to obtain a space-polarization sparse representation model of the signals;
step 4, solving the space-polarization sparse representation model to obtain a sparse vector, and extracting non-zero elements in the sparse vector;
step 5, determining the two-dimensional arrival angle of the signal through the position of the non-zero element in the orthogonal polarization redundant dictionary; meanwhile, calculating a coarse measurement value of the signal polarization angle according to the polarization components of non-zero elements in the sparse vector;
and 6, repeating the steps 3-5 to obtain rough measurement values of the two-dimensional arrival angles and the polarization angles of all signals.
2. The method for measuring the arrival angle and the polarization angle based on the polarization sensitive annular array according to claim 1, wherein in the step 2, the method for constructing the orthogonal polarization redundancy dictionary is as follows:
based on the spatial sparsity of the signal, the frequency is
Figure QLYQS_1
The two-dimensional arrival angle of the signals of (2) is discretely divided, and the number of grids is +.>
Figure QLYQS_2
Constructing an orthogonal polarization redundancy dictionary>
Figure QLYQS_3
Figure QLYQS_4
wherein ,
Figure QLYQS_5
Figure QLYQS_6
consisting of different polarization component responses of the array.
3. The method for measuring arrival angle and polarization angle based on polarization sensitive annular array according to claim 2, wherein in the step 3, the space-polarization sparse representation model of the signal:
Figure QLYQS_7
wherein ,
Figure QLYQS_8
for a frequency of +.>
Figure QLYQS_9
A spatio-polar sparse representation model of the signal of +.>
Figure QLYQS_10
For sparse vectors, ++>
Figure QLYQS_11
Representing the noise vector.
4. The method for measuring the arrival angle and the polarization angle based on the polarization-sensitive annular array according to claim 1 or 3, wherein the specific process of the step 4 is as follows: solving a space-polarization sparse representation model to obtain a sparse vector, solving non-zero elements, and converting the sparse vector into a convex optimization problem to solve in the solving process; the convex optimization problem is expressed as follows:
Figure QLYQS_12
Figure QLYQS_13
Figure QLYQS_14
wherein ,
Figure QLYQS_15
for sparse vectors, ++>
Figure QLYQS_16
For redundant dictionary->
Figure QLYQS_17
For signal vector +.>
Figure QLYQS_18
Representing the reconstruction error.
5. The method for measuring the arrival angle and the polarization angle based on the polarization-sensitive annular array according to claim 4, wherein the method for calculating the rough measurement value of the signal polarization angle in the step 5 is as follows:
Figure QLYQS_19
Figure QLYQS_20
wherein ,
Figure QLYQS_21
for the polarization angle of the signal, +.>
Figure QLYQS_22
Figure QLYQS_23
The polarization angles of the signals are respectively +.>
Figure QLYQS_24
Figure QLYQS_25
Polarization component of direction.
6. The method for measuring the arrival angle and the polarization angle based on the polarization sensitive annular array according to claim 1 or 5, further comprising a high-precision signal polarization angle measuring method, wherein the accurate measurement value of the signal polarization angle can be obtained by constructing a new polarization redundancy dictionary by uniformly and discretely dividing the polarization angle on the known signal arrival angle and performing the steps 3-5 by adopting the new polarization redundancy dictionary.
7. The polarization-sensitive annular array-based angle of arrival and polarization angle measurement method of claim 6, wherein the new polarization redundancy dictionary is:
Figure QLYQS_26
where γ represents the argument in polarization angle.
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