CN107092007A - A kind of Wave arrival direction estimating method of virtual second order array extension - Google Patents

A kind of Wave arrival direction estimating method of virtual second order array extension Download PDF

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CN107092007A
CN107092007A CN201710379098.XA CN201710379098A CN107092007A CN 107092007 A CN107092007 A CN 107092007A CN 201710379098 A CN201710379098 A CN 201710379098A CN 107092007 A CN107092007 A CN 107092007A
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mrow
msub
msubsup
msup
signal
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张瑛
王琼
汪婷静
龙政斌
赵华鹏
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University of Electronic Science and Technology of China
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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
    • G01S3/00Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/02Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
    • G01S3/14Systems for determining direction or deviation from predetermined direction
    • G01S3/143Systems for determining direction or deviation from predetermined direction by vectorial combination of signals derived from differently oriented antennae

Abstract

A kind of Wave arrival direction estimating method of virtual second order array extension of the disclosure of the invention, belong to the antenna array signals processing category for receiving wireless transmission signal, specifically, it is that one kind is directed to the method that vector is built into virtual Volterra filter constructions and carries out direction of arrival (DOA) estimation with reference to beam-forming technology and method of Lagrange multipliers technology.Vector is directed to be built into virtual Volterra filter constructions and combine beam-forming technology and method of Lagrange multipliers technology to carry out direction of arrival (DOA) estimation.This algorithm can not only realize that DOA estimates under information source number unknown condition, but also independent of Subspace Decomposition.Avoiding problems the influence that performance is produced is estimated DOA because of mistake estimation information source number, improve DOA estimation resolution capabilities, while also reducing computation complexity.

Description

A kind of Wave arrival direction estimating method of virtual second order array extension
Technical field
Category is handled the invention belongs to the antenna array signals for receiving wireless transmission signal, is that one kind will be led specifically Virtual Volterra filter constructions are built into vector and combine beam-forming technology and method of Lagrange multipliers technology to enter The method of row direction of arrival (DOA) estimation.
Background technology
In recent decades, array signal processing is as an important branch in modern signal processing field, and development is extremely Rapidly, in radar, sonar, communication, electronics, seismic prospecting, astronomical observation, biomedicine, numerous military and national economy etc. Numerous areas is widely used.And topmost two research directions of array signal processing be adaptive spatial filtering and DOA estimates.The generation of adaptive array processing technique will be estimated earlier than DOA, and be widely applied.Although on the contrary, DOA estimations are also obtaining rapid development in recent decades, during current DOA estimation theories and technology are still in developing rapidly, Turn into the main aspect of array signal processing discipline development.
Substantial amounts of DOA algorithm for estimating is suggested during this, as everyone knows by American scientist Schmidt R.O. Et al. multiple signal classification (Multiple Signal Classification, MUSIC) algorithm and Roy et al. for working out carry A kind of invariable rotary Subspace algorithm gone out.They are the once leaps in array signal processing field, realize normal resolution DOA estimation method is strided forward to subspace class super-resolution DOA estimation method.The principle of MUSIC algorithms is that autocorrelation matrix is entered Row Subspace Decomposition, obtains the noise subspace and signal subspace of matrix, then utilizes noise subspace and direction vector Orthogonality relation, estimates the incident direction of signal, and it breaches " Rayleigh limit ", with very high resolution ratio.But there is also one for it A little problems, are scanned, computationally intensive, the requirement to hardware is high if desired for all azimuths in space.In order to improve these Deficiency, it is a series of that researcher has also been proposed rooting MUSIC, space smoothing MUSIC algorithms, minimum norm, characteristic vector method etc. Noise subspace decompose space-like Power estimation algorithm.But in any case, this kind of algorithm based on signal characteristic space all must Must known information source number.Akaike information criterion and Minimum description length criterion are often used in Sources number estimation.However, experiment card It is bright under conditions of hits is less or signal to noise ratio is relatively low, these algorithms can not correctly estimate information source number.If to information source There is mistake in number estimations, and the performance of above-mentioned DOA algorithm for estimating is by degradation.In order to avoid the estimation of information source number, Wave beam forming Technology, such as minimum variance are undistorted, and response technology is also applied in DOA estimation problems.However, this beam-forming technology DOA estimations resolution ratio is not high.Afterwards, the DOA algorithm for estimating under some other unknown information source numbers is suggested, and such as uses linear prediction Or Pisarenko harmonic waves algorithm for estimating joint carries out the self-adapting signal parameter Estimation and sorting technique of DOA estimations.But this It is only to be set up in the case of information source number is less than half number of arrays to plant algorithm, and pre-estimation information source number is not also solved.For These problems are solved, a kind of new class MUSIC DOA estimation method is suggested, this algorithm avoids Subspace Decomposition, and And information source number need not be determined, so as to reduce the influence produced by Sources number estimation error to performance.
The content of the invention
The present invention seeks to be improved for existing algorithm, it is proposed that a kind of new DOA estimation method, pass through Volterra filter constructions build steering vector to carry out DOA estimations.This algorithm can not only realize information source number unknown condition Under DOA estimations, but also independent of Subspace Decomposition.Avoiding problems estimate property to DOA because of mistake estimation information source number The influence that can be produced, improves DOA estimation resolution capabilities.
The present invention solution be:It is first with Second-Order Volterra Filter, observation data configuration is new into one Array received data, and obtain a new steering vector.Then the covariance matrix of array received signal vector is estimated, The weight vector of optimal spatial filter is obtained by beam-forming technology and method of Lagrange multipliers technology again afterwards.Finally The space spectral function estimated to DOA.
The present invention is a kind of Wave arrival direction estimating method of virtual second order array extension, and this method is concretely comprised the following steps:
Step 1:New array received data y (t) is constructed by the data x (t) of array received;
Step 1-1:Without loss of generality, it is assumed that the array number of even linear array is M, information source number is P, signal incident angle difference For θ12,…,θP, then array received signal be represented by:
X (t)=As (t)+n (t)
Wherein, x (t)=[x1(t),x2(t),...,xM(t)]T,xm(t), m=1 ... M represents what m-th of array element was received Signal;A=[a (θ1),a(θ2),…,a(θP)] it is array manifold matrix,I= 1 ..., P, are the steering vector of i-th of signal source, φi=2 π dsin θi/ λ represents the phase shift of i-th of signal;Wherein d is array element Between be spaced, λ is signal wavelength, θiRepresent the arrival bearing angle of i-th of incoming signal;S (t)=[s1(t),s2..., s (t)P (t)]T, si(t) it is i-th of target source signal;N (t)=[n1(t),n2(t) ..., nM(t)]T, wherein nm(t) m-th gust is represented The additive Gaussian noise that member is received;
Step 1-2:The data of observation can obtain by Second-Order Volterra Filter:
Y (t)=Bz (t)+v (t)
In formula:
,
[·]TRepresent the transposition of matrix;xm(t), m=1,2 ..., M represent the signal that m-th of array element is received, and * represents conjugation;
,
si(t), i=1,2 ..., P are i-th of target source signal, and * represents conjugation;
,
nm(t), m=1,2 ..., M represent the additive Gaussian noise that m-th of array element is produced, and * represents conjugation;Matrix B is neotectonics Array manifold matrix;
Step 2:The new array received data y (t) obtained by step 1, constructs the steering vector of signalθi, i= 1 ..., P represent the arrival bearing angle of i-th of incoming signal, and P is information source number;
Step 3:Calculate y (t) covariance matrixyH(t) be y (t) conjugate transposition, D is Fast umber of beats;
Step 4:The y (t) obtained according to step 3 covariance matrix Ryy, calculate space spectral function P (θ);
Step 5:According to space spectral function, power spectrum chart is calculated with MATLAB, and obtains by spectrum peak search the ripple of signal Up to direction.
Further, the step 4 is concretely comprised the following steps:
Step 4-1:Can obtain a nonlinear optimization problem by beam-forming technology is:
Constraints is
Wherein,The steering vector of signal source, θ take [0 °, 180 ° be signal relative to the incident direction of normal direction, w Represent the weight vector of spatial filter, RyyThe covariance matrix of array received data newly built is represented, c, β is represented more than zero Constant;
Step 4-2:Object function is obtained using method of Lagrange multipliers:
Step 4-3:Local derviation is sought object function f (w), and makes it be equal to 0, can be obtained I is unit matrix, due toβ I are invertible matrix, thenOrderHere β=kM/ (ξ are takenM-1M- 1), k≤1, ξ1≥...≥ξP> ξP+1≥...ξM-1≥ ξMIt is RyyCharacteristic value, M is array number, can obtain Cw=η w;
Step 4-4:The characteristic value and corresponding characteristic vector for understanding to be respectively Matrix C for η and w by Cw=η w, to square Battle array C carries out Eigenvalues Decomposition, obtains M characteristic value η1≥…≥ηP> ηP+1≥…≥ηMAnd corresponding characteristic vector u1,… uP,uP+1,…uM, optimal weight vector w=u hereM
Step 4-5:Space spectral function, which can finally be obtained, is
The present invention seeks to be improved for existing algorithm, it is proposed that a kind of new DOA estimation method, be directed to arrow Amount is built into virtual Volterra filter constructions and combines beam-forming technology and method of Lagrange multipliers technology to enter traveling wave Up to direction (DOA) estimation.This algorithm can not only realize that DOA estimates under information source number unknown condition, but also independent of sub empty Between decompose.Avoiding problems the influence that performance is produced is estimated DOA because of mistake estimation information source number, improve DOA estimation resolutions Rate ability, while also reducing computation complexity.
Brief description of the drawings
Fig. 1, inventive algorithm flow chart;
The power spectrum chart of Fig. 2, the algorithm proposed compared with MUSIC algorithms and MVDR beamforming algorithms;
The curve map that Fig. 3, estimation angle root-mean-square error change with fast umber of beats.
Embodiment
Present embodiment is using array number as M=2, the uniform linear antenna array of array element spacing d=λ/2 (λ is signal wavelength) Example is classified as, and only considers two incoherent narrow band signal far field scenes, then centre frequency f is setc=70MHz, independent experiment Number of times is NMC=50.
Step 1:According to the situation of signal and antenna this body structure received, corresponding parameter is set, and utilize two Rank Volterra filter constructions construction y (t);
Step 1-1:Without loss of generality, it is assumed that the array number of even linear array is M=2, and information source number is P=2, signal incidence angle Degree is respectively θ1=30 °, θ2=33 °, then array received signal be represented by:
X (t)=As (t)+n (t)
Wherein x (t)=[x1(t),x2(t),...,xM(t)]T,xm(t), m=1 ... M represents what m-th of array element was received Signal.A=[a (θ1),a(θ2),…,a(θP)] it is array manifold matrix,I= 1 ..., P, are the steering vector of i-th of signal source, φi=2 π dsin θi/ λ represents the phase shift of i-th of signal, and wherein d is array element Between be spaced, d=λ/2, λ are signal wavelength, θiIt is the arrival bearing angle of i-th of incoming signal.S (t)=[s1(t),s2(t) ..., sP(t)]T, wherein si(t), i=1 ..., P is i-th of far field narrow band signal.The power or amplitude of signal all for 1 i.e. E | si(t) |2}=1, n (t)=[n1(t),n2(t),…,nM(t)]T, wherein nm(t), m=1 ..., M represents zero that m-th of array element is received Average white noise, if noise power is σ2, can by SNR=10log10 (E | s (t) |2}/σ2)=20dB, can obtain σ2=0.01.
Step 1-2:The data of observation are available by Second-Order Volterra Filter:
Y (t)=Bz (t)+v (t)
In formula,[·]TRepresent The transposition of matrix.x1And x (t)2(t) signal that the 1st and the 2nd array element are received is represented,Represent x2(t) conjugation.s1And s (t)2(t) it is the 1st and the 2nd target source signal.n1And n (t)2(t) the 1st is represented The additive Gaussian noise received with the 2nd array element,Represent n2(t) conjugation.Its In,I=1,2, aTi) it is a (θi) transposition,φi=2 π dsin θi/ λ, m=1 ..., M, i=1 ..., P.
It is a respectively12), a21), a22) conjugation, Re { } represents the reality of number Portion.
Step 2:WillI=1 ..., P as signal steering vector,;
Step 3:Calculate y (t) covariance matrixyH(t) be y (t) conjugate transposition, D= 100 be fast umber of beats;
Step 4:Space spectral function is tried to achieve for P (θ);
Step 4-1:It can be obtained by Wave beam forming principle:
Constraints is
Wherein it isThe steering vector of signal source, θ takes [0 °, 180 °] the incidence side for signal relative to normal direction To the sampling interval is 0.1 °, and w represents the weight vector of spatial filter, RyyRepresent the covariance square of array received data built Battle array, c represents any constant more than zero, β=kM/ (ξM-1M- 1), k≤1, ξ1≥...≥ξP> ξP+1≥...≥ξMIt is Ryy's Characteristic value, M is array number;
Step 4-2:Obtaining object function using method of Lagrange multipliers technology is:
Step 4-3:Local derviation is sought object function f (w), and makes it be equal to 0, can be obtained I is unit matrix, due toβ I are invertible matrix, thenOrderHere β=kM/ (ξ are takenM-1M- 1), k≤1, ξ1≥...≥ξP> ξP+1≥...ξM-1≥ ξMIt is RyyCharacteristic value, M is array number, can obtain Cw=η w;
Step 4-4:The characteristic value and corresponding characteristic vector for understanding to be respectively Matrix C for η and w by Cw=η w, to square Battle array C carries out Eigenvalues Decomposition, obtains M characteristic value η1≥…≥ηP> ηP+1≥…≥ηMAnd corresponding characteristic vector u1,… uP,uP+1,…uM.Here optimal weight vector w takes the characteristic vector corresponding to Matrix C minimal eigenvalue, i.e. w=uM
Step 4-5:Space spectral function, which can finally be obtained, is
Step 5:Calculated with MATLABValue, θ takes [0 °, 180 °], and with MUSIC algorithms and MVDR beamforming algorithms are compared.
Test result indicates that, as shown in Fig. 2 the figure by MUSIC algorithms, MVDR beamforming algorithms and we propose The spectrogram of algorithm, can not to tell two spaces very close for MUSIC algorithms and MVDR beamforming algorithms as seen from the figure Information source, but the algorithm that we are proposed can estimate the two information sources well, this shows that the algorithm that we are proposed is improved DOA estimates the ability of resolution ratio.Fig. 3 is the root-mean-square error (RMSE, Root-Mean-Square Error) for estimating angle The curve map changed with fast umber of beats, whereinNMC=50 be independent experiment number of times,For The deflection that ith independent experiment is estimated, θ is the incident deflection of actual signal.As seen from the figure, with the increasing of fast umber of beats Plus, estimate that the root-mean-square error of angle is less and less.

Claims (2)

1. a kind of Wave arrival direction estimating method of virtual second order array extension, this method is concretely comprised the following steps:
Step 1:New array received data y (t) is constructed by the data x (t) of array received;
Step 1-1:Without loss of generality, it is assumed that the array number of even linear array is M, and information source number is P, and signal incident angle is respectively θ1, θ2,…,θP, then array received signal be represented by:
X (t)=As (t)+n (t)
Wherein, x (t)=[x1(t),x2(t),...,xM(t)]T,xm(t), m=1 ... M represents the letter that m-th of array element is received Number;A=[a (θ1),a(θ2),…,a(θP)] it is array manifold matrix,I= 1 ..., P, are the steering vector of i-th of signal source, φi=2 π dsin θi/ λ represents the phase shift of i-th of signal;Wherein d is array element Between be spaced, λ is signal wavelength, θiRepresent the arrival bearing angle of i-th of incoming signal;S (t)=[s1(t),s2(t) ..., sP (t)]T, si(t) it is i-th of target source signal;N (t)=[n1(t),n2(t) ..., nM(t)]T, wherein nm(t) m-th gust is represented The additive Gaussian noise that member is received;
Step 1-2:The data of observation can obtain by Second-Order Volterra Filter:
Y (t)=Bz (t)+v (t)
In formula:
<mfenced open = "" close = ""> <mtable> <mtr> <mtd> <mrow> <mi>y</mi> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>=</mo> <mo>&amp;lsqb;</mo> <msub> <mi>x</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>x</mi> <mi>M</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <msubsup> <mi>x</mi> <mn>1</mn> <mn>2</mn> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <msubsup> <mi>x</mi> <mi>M</mi> <mn>2</mn> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mo>|</mo> <msub> <mi>x</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msup> <mo>|</mo> <mn>2</mn> </msup> <mo>,</mo> <mn>...</mn> <mo>|</mo> <msub> <mi>x</mi> <mi>M</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msup> <mo>|</mo> <mn>2</mn> </msup> <mo>,</mo> <msub> <mi>x</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>x</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>x</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>x</mi> <mi>M</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <msub> <mi>x</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>x</mi> <mn>3</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>x</mi> <mrow> <mi>M</mi> <mo>-</mo> <mn>1</mn> </mrow> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>x</mi> <mi>M</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> </mrow> </mtd> </mtr> <mtr> <mtd> <mrow> <msub> <mi>x</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>x</mi> <mn>2</mn> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>x</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>x</mi> <mi>M</mi> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>x</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>x</mi> <mn>3</mn> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>x</mi> <mrow> <mi>M</mi> <mo>-</mo> <mn>1</mn> </mrow> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>x</mi> <mi>M</mi> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msup> <mo>&amp;rsqb;</mo> <mi>T</mi> </msup> </mrow> </mtd> </mtr> </mtable> </mfenced> ,
[·]TRepresent the transposition of matrix;xm(t), m=1,2 ..., M represent the signal that m-th of array element is received, and * represents conjugation;
<mfenced open = "" close = ""> <mtable> <mtr> <mtd> <mrow> <mi>z</mi> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>=</mo> <mo>&amp;lsqb;</mo> <msub> <mi>s</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mo>...</mo> <mo>,</mo> <msub> <mi>s</mi> <mi>P</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <msubsup> <mi>s</mi> <mn>1</mn> <mn>2</mn> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mo>...</mo> <msubsup> <mi>s</mi> <mi>P</mi> <mn>2</mn> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <msub> <mi>s</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>s</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mo>...</mo> <mo>,</mo> <msub> <mi>s</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>s</mi> <mi>P</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <msub> <mi>s</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>s</mi> <mn>3</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>s</mi> <mrow> <mi>P</mi> <mo>-</mo> <mn>1</mn> </mrow> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>s</mi> <mi>P</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <msub> <mi>s</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>s</mi> <mn>2</mn> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>s</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>s</mi> <mi>P</mi> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> </mrow> </mtd> </mtr> <mtr> <mtd> <mrow> <mn>...</mn> <mo>,</mo> <msub> <mi>s</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>s</mi> <mn>3</mn> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>s</mi> <mrow> <mi>P</mi> <mo>-</mo> <mn>1</mn> </mrow> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>s</mi> <mi>P</mi> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <msubsup> <mi>s</mi> <mn>1</mn> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>s</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msubsup> <mi>s</mi> <mn>1</mn> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>s</mi> <mi>P</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <msubsup> <mi>s</mi> <mn>2</mn> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>s</mi> <mn>3</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msubsup> <mi>s</mi> <mrow> <mi>P</mi> <mo>-</mo> <mn>1</mn> </mrow> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>s</mi> <mi>P</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msup> <mo>&amp;rsqb;</mo> <mi>T</mi> </msup> </mrow> </mtd> </mtr> </mtable> </mfenced> ,
si(t), i=1,2 ..., P are i-th of target source signal, and * represents conjugation;
<mfenced open = "" close = ""> <mtable> <mtr> <mtd> <mrow> <mi>v</mi> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>=</mo> <mo>&amp;lsqb;</mo> <msub> <mi>n</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mo>...</mo> <mo>,</mo> <msub> <mi>n</mi> <mi>M</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <msubsup> <mi>n</mi> <mn>1</mn> <mn>2</mn> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mo>...</mo> <msubsup> <mi>n</mi> <mi>M</mi> <mn>2</mn> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mo>|</mo> <msub> <mi>n</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msup> <mo>|</mo> <mn>2</mn> </msup> <mo>,</mo> <mn>...</mn> <mo>|</mo> <msub> <mi>n</mi> <mi>M</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msup> <mo>|</mo> <mn>2</mn> </msup> <mo>,</mo> <msub> <mi>n</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>n</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>n</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>n</mi> <mi>M</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <msub> <mi>n</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>n</mi> <mn>3</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>n</mi> <mrow> <mi>M</mi> <mo>-</mo> <mn>1</mn> </mrow> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msub> <mi>n</mi> <mi>M</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> </mrow> </mtd> </mtr> <mtr> <mtd> <mrow> <msub> <mi>n</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>n</mi> <mn>2</mn> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>n</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>n</mi> <mi>M</mi> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>n</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>n</mi> <mn>3</mn> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>,</mo> <mn>...</mn> <mo>,</mo> <msub> <mi>n</mi> <mrow> <mi>M</mi> <mo>-</mo> <mn>1</mn> </mrow> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msubsup> <mi>n</mi> <mi>M</mi> <mo>*</mo> </msubsup> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <msup> <mo>&amp;rsqb;</mo> <mi>T</mi> </msup> </mrow> </mtd> </mtr> </mtable> </mfenced> ,
nm(t), m=1,2 ..., M represent the additive Gaussian noise that m-th of array element is produced, and * represents conjugation;Matrix B is neotectonics Array manifold matrix;
Step 2:The new array received data y (t) obtained by step 1, constructs the steering vector of signalθi, i= 1 ..., P represent the arrival bearing angle of i-th of incoming signal, and P is information source number;
Step 3:Calculate y (t) covariance matrixyH(t) be y (t) conjugate transposition, D is snap Number;
Step 4:The y (t) obtained according to step 3 covariance matrix Ryy, calculate space spectral function P (θ);
Step 5:According to space spectral function, power spectrum chart is calculated with MATLAB, and the ripple for obtaining signal by spectrum peak search reaches side To.
2. a kind of Wave arrival direction estimating method of virtual second order array extension as claimed in claim 1, it is characterised in that described Step 4 is concretely comprised the following steps:
Step 4-1:Can obtain a nonlinear optimization problem by beam-forming technology is:
Constraints is
Wherein,The steering vector of signal source, θ take [0 °, 180 °] for signal relative to the incident direction of normal direction, w tables Show the weight vector of spatial filter, RyyThe covariance matrix of array received data newly built is represented, c, β represents normal more than zero Amount;
Step 4-2:Object function is obtained using method of Lagrange multipliers:
<mrow> <mi>f</mi> <mrow> <mo>(</mo> <mi>w</mi> <mo>)</mo> </mrow> <mo>=</mo> <msup> <mi>w</mi> <mi>H</mi> </msup> <msub> <mi>R</mi> <mrow> <mi>y</mi> <mi>y</mi> </mrow> </msub> <mi>w</mi> <mo>-</mo> <mi>&amp;eta;</mi> <mrow> <mo>(</mo> <msup> <mi>w</mi> <mi>H</mi> </msup> <mover> <mi>B</mi> <mo>~</mo> </mover> <mo>(</mo> <mi>&amp;theta;</mi> <mo>)</mo> <msup> <mover> <mi>B</mi> <mo>~</mo> </mover> <mi>H</mi> </msup> <mo>(</mo> <mi>&amp;theta;</mi> <mo>)</mo> <mi>w</mi> <mo>+</mo> <mi>&amp;beta;</mi> <mo>|</mo> <mo>|</mo> <mi>w</mi> <mo>|</mo> <msubsup> <mo>|</mo> <mn>2</mn> <mn>2</mn> </msubsup> <mo>-</mo> <mi>c</mi> <mo>)</mo> </mrow> </mrow>
Step 4-3:Local derviation is sought object function f (w), and makes it be equal to 0, can be obtainedI is single Bit matrix, due toFor invertible matrix, thenOrder Here β=kM/ (ξ are takenM-1M- 1), k≤1, ξ1≥...≥ξP> ξP+1≥...ξM-1≥ξMIt is RyyCharacteristic value, M is array element Number, can obtain Cw=η w;
Step 4-4:The characteristic value and corresponding characteristic vector for understanding to be respectively Matrix C for η and w by Cw=η w, enter to Matrix C Row Eigenvalues Decomposition, obtains M characteristic value η1≥…≥ηP> ηP+1≥…≥ηMAnd corresponding characteristic vector u1,…uP, uP+1,…uM, optimal weight vector w=u hereM
Step 4-5:Space spectral function, which can finally be obtained, is
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CN111884689B (en) * 2020-07-10 2021-10-22 中国科学技术大学 Direction-of-arrival-distance adaptive beam forming method based on ladder array
CN111884689A (en) * 2020-07-10 2020-11-03 中国科学技术大学 Direction-of-arrival-distance adaptive beam forming method based on ladder array
CN112924926A (en) * 2021-01-27 2021-06-08 东南大学 DOA estimation method under multi-path channel
CN113420411A (en) * 2021-05-25 2021-09-21 北京科技大学 High-resolution narrowband DOA estimation algorithm for wireless signals and implementation method
CN113420411B (en) * 2021-05-25 2024-02-20 北京科技大学 High-resolution narrowband DOA estimation algorithm for wireless signals and implementation method
CN114563760A (en) * 2022-02-07 2022-05-31 哈尔滨工程大学 Second-order super-beam forming method, equipment and medium based on SCA array type
CN114563760B (en) * 2022-02-07 2023-02-07 哈尔滨工程大学 Second-order super-beam forming method, equipment and medium based on SCA array

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Application publication date: 20170825