CN112230226B - Adaptive beam former design method based on Bayes compressed sensing algorithm - Google Patents

Adaptive beam former design method based on Bayes compressed sensing algorithm Download PDF

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CN112230226B
CN112230226B CN202011009033.4A CN202011009033A CN112230226B CN 112230226 B CN112230226 B CN 112230226B CN 202011009033 A CN202011009033 A CN 202011009033A CN 112230226 B CN112230226 B CN 112230226B
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CN112230226A (en
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陈耀武
林振伟
刘雪松
蒋荣欣
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Zhejiang University ZJU
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S15/00Systems using the reflection or reradiation of acoustic waves, e.g. sonar systems
    • G01S15/88Sonar systems specially adapted for specific applications
    • G01S15/89Sonar systems specially adapted for specific applications for mapping or imaging
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/52Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S15/00
    • G01S7/52001Auxiliary means for detecting or identifying sonar signals or the like, e.g. sonar jamming signals
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/52Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S15/00
    • G01S7/539Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S15/00 using analysis of echo signal for target characterisation; Target signature; Target cross-section

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Abstract

The invention discloses a design method of an adaptive beam former based on a Bayesian compressed sensing algorithm, which comprises the following steps: (1) The planar array elements receive sound wave incident signals, the sound wave incident signals comprise target signals and interference signals, an adaptive beam former is constructed on the basis of the sound wave incident signals, and the arrival direction of the sound wave incident signals is estimated by adopting a Bayesian compression sensing algorithm; (2) Obtaining an interference plus noise covariance matrix according to the direction of arrival of the interference signal and Capon space spectrum reconstruction of the incident sound wave signal; (3) And defining a maximum sidelobe level constraint value, constraining sidelobes of the target beam pattern according to the maximum sidelobe level constraint value, and calculating an array element weight coefficient of the self-adaptive beam former through a convex optimization method according to an interference and noise covariance matrix. With a greater output signal-to-dry ratio.

Description

Adaptive beam former design method based on Bayes compressed sensing algorithm
Technical Field
The invention relates to the field of sonar array signal processing, in particular to a design method of an adaptive beam former based on a Bayesian compressed sensing algorithm (BCS).
Background
In recent years, phased array three-dimensional imaging sonar technology has been rapidly developed due to its application to underwater physics, biology, geology, and the like. The traditional phased array three-dimensional sonar has a fixed beam direction, cannot automatically track the incoming direction of a desired signal while cancelling interference, and cannot meet the working requirement in a complex underwater acoustic environment, for example, a patent application with application publication number CN109116334A discloses a sonar beam forming method and system based on super-beam weighting.
The adaptive beam forming algorithm is used as a new technical means, and on the premise of ensuring the large gain reception of the expected signal, the beam pattern null is adaptively aligned to the interference direction, so that the adaptive control on the beam pattern of the array is realized, and the interference is suppressed or the intensity of the interference signal is reduced. Therefore, it is of great significance to study adaptive beamforming algorithms. For example, patent application with publication number CN110736976A discloses a method for estimating the performance of sonar beam former in any array. Patent application publication No. CN110196421A discloses a dense-distributed MIMO sonar adaptive beam forming detection method.
Disclosure of Invention
The invention aims to provide a design method of an adaptive beam former based on a Bayes compressed sensing algorithm, which realizes more accurate reconstruction of an interference plus noise covariance matrix through the Bayes compressed sensing algorithm, has a larger output signal-to-noise ratio compared with other adaptive algorithms, and is also restricted to a lower level by sidelobe peaks of a beam pattern.
In order to realize the purpose of the invention, the technical scheme provided by the invention is as follows:
a design method of an adaptive beam former based on a Bayesian compressed sensing algorithm comprises the following steps:
(1) The planar array elements receive sound wave incident signals, the sound wave incident signals comprise target signals and interference signals, an adaptive beam former is constructed on the basis of the sound wave incident signals, and the arrival direction of the sound wave incident signals is estimated by adopting a Bayesian compression sensing algorithm;
(2) Obtaining an interference and noise covariance matrix according to the direction of arrival of the interference signal and Capon space spectrum reconstruction of the sound wave incident signal;
(3) Defining a maximum sidelobe level (PSLL) constraint value, constraining sidelobes of a target beam pattern according to the maximum sidelobe level constraint value, and calculating a weight coefficient value of the adaptive beam former through a convex optimization method according to an interference and noise covariance matrix.
In step (1), the received sound wave incident signal is expressed as:
Figure BDA0002696954570000021
wherein k represents the number of fast sampling beats, and X (k) represents the number of fast sampling beatsA received acoustic incident signal at k, n (k) representing a Gaussian noise vector, s (k) = [ s = [ k ] l (k),l=1,2,...,L] T An incident signal source indicating L +1 directions, L indicating an index of the incident direction, and (α) when L =0 l ,β l ) Represents the incident direction of the target signal, and when L =1,2 l ,β l ) Indicates the incident direction of the interference signal, a (α) l ,β l ) Indicates an incident direction of (alpha) l ,β l ) Of phi = [ a (alpha) ] l ,β l ),l=1,2,...,L]And expressing the array manifold matrix, specifically as follows:
Figure BDA0002696954570000031
wherein λ is the wavelength, x n ,y n Denotes the position of the nth array element, N =1,2 l =sinα l ,v l =sinβ l ,u l ,u l ∈[-1,1]L =1,2,. Wherein L, L is a natural number;
constructing an adaptive beamformer based on acoustic incident signals is represented as:
Y(k)=w H X(k) (3)
where Y (k) represents the output of the adaptive beamformer, w H ∈C N Representing array element weight coefficients, superscript H Representing the Hermite transpose, the output signal-to-interference-plus-noise ratio (SINR) of the adaptive beamformer can be calculated as follows:
Figure BDA0002696954570000032
wherein, E [. C]Denotes expectation, | 2 Denotes the square, X s (k),X i (k) And X n (k) Representing the target signal component, the interference signal component and the noise component, σ, respectively s 2 Representing the energy of the signal, a s Array manifold vector, R, representing a target signal i+n =E[(X i (k)+X n (k)(X i (k)+X n (k) H ]∈C N×N Representing the interference plus noise covariance matrix, the design of the adaptive beamformer turns into the following problem:
min w w H R i+n w,subject to w H a s =1. (5)
when the Bayes compressed sensing algorithm is adopted to estimate the direction of arrival (DOA) of the sound wave incident signal, the number of candidate signal directions is set to be M, and then the candidate signal source can be expressed as
Figure BDA0002696954570000033
Figure BDA0002696954570000034
The sound wave incident signal received by the array element
Figure BDA0002696954570000035
The rewrite is:
Figure BDA0002696954570000036
wherein,
Figure BDA0002696954570000037
which represents the vector of the noise, is,
Figure BDA0002696954570000038
representing candidate signal source vectors, array manifold matrices
Figure BDA0002696954570000039
As follows:
Figure BDA0002696954570000041
the DOA estimation problem can be transformed as follows:
Figure BDA0002696954570000042
wherein Q = R, I,
Figure BDA0002696954570000043
and
Figure BDA0002696954570000044
respectively representing candidate signal sources
Figure BDA0002696954570000045
The real and imaginary parts of (a) and (b),
Figure BDA0002696954570000046
represents the posterior probability, then
Figure BDA0002696954570000047
Comprises the following steps:
Figure BDA0002696954570000048
Figure BDA0002696954570000049
Figure BDA00026969545700000410
wherein R (-) denotes taking the real part, I (-) denotes taking the imaginary part, ε (k) is a fidelity coefficient, and represents the accuracy of the DOA estimation of the signal,
Figure BDA00026969545700000411
posterior probability
Figure BDA00026969545700000412
Introduction of hyper-parameters
Figure BDA00026969545700000413
Conversion to:
Figure BDA00026969545700000414
wherein Q = R, I, R, I respectively represent a real part and an imaginary part, and a hyperparameter
Figure BDA00026969545700000415
The value of (d) is obtained by solving its maximum likelihood function, as follows:
Figure BDA00026969545700000416
wherein Q = R, I, a and b are user-defined proportion control parameters,
Figure BDA00026969545700000417
is shown in
Figure BDA0002696954570000051
For diagonal matrices of diagonal elements, superscript T Represents a transpose of a matrix; the DOA estimate of the incident acoustic signal can be obtained by:
Figure BDA0002696954570000052
due to the fact that
Figure BDA0002696954570000053
There are K samples and the derivation above uses only one of the samples. When DOA estimation is carried out through a multitask Bayes compressed sensing algorithm (MT-BCS), K sampling points can be associated by sharing the same hyper-parameter and observation matrix, so that the estimation precision is improved, and the DOA estimation in the formula (14) can be written as follows:
Figure BDA0002696954570000054
when the incident direction index l =0, the direction of arrival of the target signal is obtained according to equation (15), and when the incident direction index l ≠ 0, the direction of arrival of the interference signal is obtained according to equation (15).
In the step (2), the direction of arrival obtained in the step (1) can be divided into the incident direction of the target signal source as (u) according to the prior information of the target signal azimuth 0 ,v 0 ) The corresponding array manifold vector is
Figure BDA0002696954570000055
And the incident direction of the interfering signal source is (u) l ,v l ) (L =1,2, \8230;, L), corresponding to an array manifold vector of
Figure BDA0002696954570000056
The spatial spectrum function of the sound wave incident signal Capon is as follows:
Figure BDA0002696954570000057
wherein,
Figure BDA0002696954570000058
the sampling covariance matrix of the array element is represented, and the interference-plus-noise covariance matrix is reconstructed according to the arrival direction of the interference signal
Figure BDA0002696954570000059
The following:
Figure BDA00026969545700000510
in step (3), defining a maximum side lobe level (PSLL) constraint value as BP PSLL Let (u) j ,v j ) (J =1,2, \8230;, J) denotes the side lobe region of the target beam pattern, the side lobe constraints are as follows:
Figure BDA00026969545700000511
interference plus noise covariance matrix incorporating reconstruction
Figure BDA0002696954570000061
Then the array element coefficients of the adaptive beam former are solved by a convex optimization method to obtain the weight coefficient values of the adaptive beam former, and the solving process is as follows:
Figure BDA0002696954570000062
subject to
Figure BDA0002696954570000063
Figure BDA0002696954570000064
after obtaining the weight coefficient values of the adaptive beamformer, the values can be determined according to Y (k) = w H X (k) results in an adaptive beamformer.
The maximum side lobe level (PSLL) constraint value is related to the aperture of the array and the number of the array elements, and the maximum side lobe level (PSLL) constraint value is set according to the aperture of the array and the number of the array elements, and the more the array elements are, the smaller the side lobe is. For example, for a 20 x 20 array, the maximum side lobe level (PSLL) constraint value is-25 dB, and no solution is found when the constraint value is less than-25.
Compared with the prior art, the invention has the beneficial effects that:
according to the method, a Bayes compressed sensing algorithm carries out DOA estimation on sound wave incident signals received by an array element to obtain the directions of a target signal source and an interference signal source, and an interference plus noise covariance matrix can be accurately reconstructed according to the obtained directions of the target signal source and the interference signal source and combined with Capon space spectrum estimation of sampled data. Meanwhile, compared with other adaptive beam forming algorithms, the adaptive beam former provided by the invention restricts the sidelobe of a beam pattern and controls the sidelobe at a lower level. The method realizes more accurate reconstruction of the interference and noise covariance matrix, and has a larger output signal-to-noise ratio and a better side lobe control level.
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In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the embodiments or the description of the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to these drawings without creative efforts.
FIG. 1 is a schematic view of the azimuth definition of the adaptive beamformer design method based on the Bayesian compressive sensing algorithm according to the present invention;
FIG. 2 is a schematic diagram of the signal source and the direction and intensity of an interference source of the adaptive beamformer design method based on the Bayesian compressive sensing algorithm of the present invention;
fig. 3 is a beam diagram of the adaptive beamformer design method based on the bayesian compressive sensing algorithm according to the present invention.
FIG. 4 is a graph comparing the performance of the present invention with other methods at different input signal-to-noise ratios.
Fig. 5 is a graph comparing the performance of the present invention with other methods at different sampling times.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be further described in detail with reference to the accompanying drawings and examples. It should be understood that the detailed description and specific examples, while indicating the scope of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.
The invention provides a design method of an adaptive beam former based on a Bayes compressed sensing algorithm, which realizes more accurate reconstruction of an interference and noise covariance matrix through the Bayes compressed sensing algorithm, has a larger output signal-to-noise ratio compared with other adaptive algorithms, and is also restricted at a lower level by a side lobe peak value of a beam pattern.
In this embodiment, the design is considered to be a 20 x 20 two-dimensional transducer array. Fig. 1 is a schematic azimuth angle definition diagram of the adaptive beamformer design method based on the bayesian compressed sensing algorithm of the present invention, wherein α and β represent the angles of the incident acoustic wave signals in the horizontal and vertical directions. Assuming that the signal incidence direction is (0 ° ), the two interference source incidence directions are (45 °,36 °) and (30 °,60 °) respectively, and the input interference-to-noise ratio (INR) is 30dB. The transducers are uniformly distributed in a rectangular plane according to the half-wavelength distance, the horizontal and vertical distances of the transducers are equal, the carrier frequency is f =300kHz, the sound velocity is 1500m/s, the value ranges of u and v are (-1, 1) and (-1, 1) respectively, and the beam number is 181 multiplied by 181.
The embodiment provides a design method of an adaptive beam former based on a Bayesian compressed sensing algorithm, which comprises the following specific steps:
step 1, the number of candidate signal directions is M =181 × 181, and the candidate signal source can be represented as
Figure BDA0002696954570000081
The signal received by the array element can be rewritten as:
Figure BDA0002696954570000082
wherein, the array manifold matrix is as follows:
Figure BDA0002696954570000083
the DOA estimation problem can be transformed as follows:
Figure BDA0002696954570000084
wherein,
Figure BDA0002696954570000085
and
Figure BDA0002696954570000086
respectively represent
Figure BDA0002696954570000087
The real and imaginary parts of (a) and (b),
Figure BDA0002696954570000088
the posterior probability is expressed. Then
Figure BDA0002696954570000089
Comprises the following steps:
Figure BDA00026969545700000810
Figure BDA00026969545700000811
Figure BDA00026969545700000812
where ε (k) is the fidelity coefficient representing the accuracy of the signal DOA estimate. Posterior probability
Figure BDA00026969545700000813
Introduction of hyper-parameters
Figure BDA00026969545700000814
Conversion to:
Figure BDA00026969545700000815
wherein R and I respectively represent real part and imaginary part, and hyperparameter
Figure BDA0002696954570000091
The value of (a) is obtained by solving its maximum likelihood function,as follows:
Figure BDA0002696954570000092
wherein a and b are user-defined proportional control parameters,
Figure BDA0002696954570000093
is shown in
Figure BDA0002696954570000094
A diagonal matrix being diagonal elements; the DOA of the incident signal can be found by:
Figure BDA0002696954570000095
the resulting orientations and normalized intensities of the signal source and the interference source are shown in fig. 2.
Step 2, according to the obtained direction of the incident signal source, the direction is (0 degree ), and the array manifold vector is
Figure BDA0002696954570000096
The interference sources are oriented at (45, 36) and (30, 60) degrees, and the array manifold vector is
Figure BDA0002696954570000097
Capon spatial spectrum function is:
Figure BDA0002696954570000098
wherein,
Figure BDA0002696954570000099
a sampled covariance matrix representing array elements. The interference plus noise covariance matrix can be reconstructed as follows:
Figure BDA00026969545700000910
and 3, setting the peak value of the side lobe to be-25 dB, and solving the array element coefficient of the adaptive beam former by a convex optimization method. The resulting beam pattern is shown in fig. 3, and compared with other adaptive beamforming algorithms, including the diagonal loading method (DL), the worst case method (WC), the direct inversion method (SMI), and the covariance matrix reconstruction method (CMR), is shown in fig. 4 and 5, where fig. 4 compares the output signal-to-interference ratio (SINR) at different input signal-to-noise ratios (SNR), and fig. 5 compares the output signal-to-interference ratio (SINR) at different sampling times. It can be seen that the performance of the present invention is always superior to other methods under different conditions.
The technical solutions and advantages of the present invention have been described in detail in the foregoing detailed description, and it should be understood that the above description is only the most preferred embodiment of the present invention, and is not intended to limit the present invention, and any modifications, additions, and equivalents made within the scope of the principles of the present invention should be included in the protection scope of the present invention.

Claims (4)

1. A design method of an adaptive beam former based on a Bayesian compressed sensing algorithm is characterized by comprising the following steps:
(1) The planar array element receives an acoustic wave incident signal, the acoustic wave incident signal comprises a target signal and an interference signal, and an adaptive beam former is constructed based on the acoustic wave incident signal, wherein the received acoustic wave incident signal is represented as:
Figure FDA0003851445340000011
where k denotes a sampling fast beat number, X (k) denotes an acoustic wave incident signal received when the sampling fast beat number is k, n (k) denotes a gaussian noise vector, and s (k) = [ s ] - [ s ] l (k),l=0,1,2,...,L] T An incident signal source indicating L +1 directions, L indicating an index of the incident direction, and (α) when L =0 l ,β l ) Indicating the direction of incidence of the target signal, when l =1,2.,when is equal to (alpha) l ,β l ) Indicates the incident direction of the interference signal, a (alpha) l ,β l ) Indicates an incident direction of (alpha) l ,β l ) Of phi = [ a (alpha) ] l ,β l ),l=0,1,2,...,L]And expressing the array manifold matrix, specifically as follows:
Figure FDA0003851445340000012
wherein λ is the wavelength, x n ,y n Denotes the position of the nth array element, N =1,2 l =sinα l ,v l =sinβ l L =0,1,2, ·, L is a natural number;
constructing an adaptive beamformer based on acoustic incident signals is represented as:
Y(k)=w H X(k) (3)
where Y (k) represents the output of the adaptive beamformer, w H ∈C N Representing array element weight coefficients, and superscript H representing a Hermite transpose;
estimating the direction of arrival of the incident sound wave signals by adopting a Bayesian compressed sensing algorithm, and when estimating the direction of arrival of the incident sound wave signals by adopting the Bayesian compressed sensing algorithm, making the number of candidate signal directions M, and then expressing the candidate signal sources as M
Figure FDA0003851445340000021
Then the acoustic incident signal received by the array element is rewritten as:
Figure FDA0003851445340000022
wherein,
Figure FDA0003851445340000023
representing the incident signal of the acoustic wave being overwritten,
Figure FDA0003851445340000024
the representation of the noise vector is carried out,
Figure FDA0003851445340000025
representing candidate signal source vectors, array manifold matrices
Figure FDA0003851445340000026
As follows:
Figure FDA0003851445340000027
the direction of arrival estimation problem translates to the following:
Figure FDA0003851445340000028
wherein,
Figure FDA0003851445340000029
and
Figure FDA00038514453400000210
respectively representing candidate signal sources
Figure FDA00038514453400000211
The real and imaginary parts of (a) and (b),
Figure FDA00038514453400000212
represents the posterior probability, then
Figure FDA00038514453400000213
Comprises the following steps:
Figure FDA00038514453400000214
Figure FDA00038514453400000215
Figure FDA00038514453400000216
wherein R (-) denotes taking the real part, I (-) denotes taking the imaginary part, ε (k) is a fidelity coefficient, and represents the accuracy of the DOA estimation of the signal,
Figure FDA00038514453400000217
posterior probability
Figure FDA00038514453400000218
Introducing a hyperparameter
Figure FDA00038514453400000219
Conversion to:
Figure FDA00038514453400000220
wherein Q = R, I, R, I respectively represent a real part and an imaginary part, and a hyperparameter
Figure FDA00038514453400000221
The value of (d) is obtained by solving its maximum likelihood function, as follows:
Figure FDA0003851445340000031
wherein Q = R, I, a and b are user-defined proportion control parameters,
Figure FDA0003851445340000032
is shown in
Figure FDA0003851445340000033
A superscript T represents the transpose of the matrix for a diagonal matrix of diagonal elements; the DOA estimate of the acoustic incident signal is then obtained by:
Figure FDA0003851445340000034
Figure FDA0003851445340000035
when the direction of arrival estimation is performed through a multi-task Bayes compressed sensing algorithm, K sampling points are associated by sharing the same hyper-parameter and observation matrix, so that the direction of arrival estimation in the formula (12) is written as follows:
Figure FDA0003851445340000036
when the incident direction index l =0, obtaining the direction of arrival of the target signal according to a formula (13), and when the incident direction index l ≠ 0, obtaining the direction of arrival of the interference signal according to the formula (13);
(2) Obtaining an interference-plus-noise covariance matrix according to the direction of arrival of the interference signal and Capon space spectrum reconstruction of the incident signal of the acoustic wave
Figure FDA0003851445340000037
(3) Defining a maximum sidelobe level constraint value as BP PSLL Order (u) j ,v j ) Represents the sidelobe region of the target beam pattern, where J =1, 2.. And J, then the sidelobes of the target beam pattern are constrained according to a maximum sidelobe level constraint value, which is expressed as:
Figure FDA0003851445340000038
wherein the reconstructed interference-plus-noise covariance matrix is combined
Figure FDA0003851445340000039
Then the array element coefficients of the adaptive beam former are solved by a convex optimization method to obtain the weight coefficient values of the adaptive beam former, and the solving process is as follows:
Figure FDA0003851445340000041
Figure FDA0003851445340000042
Figure FDA0003851445340000043
after obtaining the weight coefficient values of the adaptive beamformer, i.e. according to Y (k) = w H X (k) results in an adaptive beamformer.
2. The adaptive beamformer design method based on the bayesian compressed sensing algorithm according to claim 1, wherein the output signal to interference plus noise ratio SINR of the adaptive beamformer is calculated as follows:
Figure FDA0003851445340000044
wherein, E [. C]Denotes expectation, | 2 Represents the square, X s (k),X i (k) And X n (k) Respectively representing a target signal component, an interference signal component and a noise component, sigma s 2 Representing the energy of the signal, a s Array manifold vector, R, representing target signal i+n =E[(X i (k)+X n (k))(X i (k)+X n (k)) H ]∈C N×N Representing the interference plus noise covariance matrix, the design of the adaptive beamformer turns into the following problem:
min w w H R i+n w,subject to w H a s =1 (19)。
3. the adaptive beamformer design method based on Bayesian compressive sensing algorithm as claimed in claim 1, wherein in step (2), the sound wave incident signal Capon spatial spectrum function
Figure FDA0003851445340000045
Comprises the following steps:
Figure FDA0003851445340000046
wherein,
Figure FDA0003851445340000047
a sampling covariance matrix representing the array elements;
the interference-plus-noise covariance matrix reconstructed from the direction of arrival of the interfering signal
Figure FDA0003851445340000048
The following were used:
Figure FDA0003851445340000051
wherein,
Figure FDA0003851445340000052
indicating the direction of incidence (u) of the interfering signal source l ,v l ) A corresponding array manifold vector.
4. The adaptive beamformer design method based on the Bayesian compressed sensing algorithm as recited in claim 1, wherein a maximum sidelobe level constraint value is set according to an aperture of an array and the number of array elements, and sidelobes are smaller as array elements are larger.
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