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CN102608598A - Method for imaging actual aperture foresight on basis of subspace projection - Google Patents

Method for imaging actual aperture foresight on basis of subspace projection Download PDF

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CN102608598A
CN102608598A CN2012100725990A CN201210072599A CN102608598A CN 102608598 A CN102608598 A CN 102608598A CN 2012100725990 A CN2012100725990 A CN 2012100725990A CN 201210072599 A CN201210072599 A CN 201210072599A CN 102608598 A CN102608598 A CN 102608598A
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杨志伟
廖桂生
杨凯新
刘笑菲
曾操
何嘉懿
夏桂琴
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Xidian University
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Abstract

本发明公开了一种基于子空间投影的实孔径前视成像方法,主要解决飞行轨迹正前方目标的高分辨成像问题。其检测过程为:1)等间距发射雷达波束,对地面监视区域进行顺序重叠扫描,获取雷达回波数据;2)通过取模运算,提取回波数据的强度矢量;3)求取回波强度矢量的自相关矩阵;4)对自相关矩阵进行特征分解;5)用小特征值对应的特征向量构造噪声子空间;6)定义方向图搜索矢量;7)将方向图搜索矢量投影到噪声子空间上;8)计算空间谱函数的峰值;9)根据空间谱函数峰值的数目确定信号的个数,实现前视成像。本发明具有提高主瓣内邻近目标分辨精度的优点,可用于机载雷达监视系统实现航迹线方向目标检测与识别的成像领域。

Figure 201210072599

The invention discloses a real-aperture forward-looking imaging method based on subspace projection, which mainly solves the problem of high-resolution imaging of a target directly in front of a flight track. The detection process is as follows: 1) Emitting radar beams at equal intervals, sequentially overlapping scanning of the ground surveillance area, and obtaining radar echo data; 2) Extracting the intensity vector of the echo data through modulo calculation; 3) Obtaining the echo intensity Vector autocorrelation matrix; 4) Eigendecompose the autocorrelation matrix; 5) Construct the noise subspace with the eigenvector corresponding to the small eigenvalue; 6) Define the pattern search vector; 7) Project the pattern search vector to the noise subspace In space; 8) calculating the peak value of the spatial spectral function; 9) determining the number of signals according to the peak value of the spatial spectral function to realize forward-looking imaging. The invention has the advantage of improving the resolution accuracy of the adjacent targets in the main lobe, and can be used in the imaging field of the airborne radar monitoring system to realize the detection and identification of the target in the track line direction.

Figure 201210072599

Description

基于子空间投影的实孔径前视成像方法Real Aperture Front-Look Imaging Method Based on Subspace Projection

技术领域 technical field

本发明涉及成像领域,特别涉及飞行轨迹正前方目标的高分辨成像问题,可用于机载雷达监视系统对沿航迹线方向的目标进行检测与识别。The invention relates to the field of imaging, in particular to the problem of high-resolution imaging of a target directly in front of a flight track, which can be used in an airborne radar monitoring system to detect and identify targets along the direction of the flight track.

背景技术 Background technique

在未来瞬息万变的现代化高科技战争环境中,战场信息复杂多变,战机转瞬即逝,及时、正确地进行战场检测和战术侦察关系到战争的成败。因此,必然要求雷达成像系统具有一定的成像精度和成像范围。但是,当天线波束与航迹线接近重合时,由于分布在航迹两侧的地面目标具有相同的多普勒历程容易发生混叠,且目标的多普勒变化率很小,方位分辨率会迅速下降,形成前视“盲区”,而现有的合成孔径雷达系统无法解决这一问题。因此,如何更好地利用雷达系统对正前方目标实施有效的侦查,以获取前视图像已成为雷达界研究的热点之一。In the ever-changing modern high-tech warfare environment in the future, battlefield information is complex and changeable, and fighters are fleeting. Timely and correct battlefield detection and tactical reconnaissance are related to the success or failure of the war. Therefore, it is necessary to require the radar imaging system to have a certain imaging accuracy and imaging range. However, when the antenna beam is close to coincident with the track line, since the ground targets distributed on both sides of the track have the same Doppler history, aliasing is likely to occur, and the Doppler change rate of the target is very small, the azimuth resolution will be reduced. Rapid decline, forming a forward-looking "blind zone", and the existing synthetic aperture radar system cannot solve this problem. Therefore, how to better use the radar system to carry out effective detection of the target in front to obtain the forward-looking image has become one of the hotspots in the radar field.

针对前视成像问题,典型的解决方案有:双基地SAR前视成像方法,单脉冲前视成像方法,实孔径解卷积前视成像方法等,其中:For the forward-looking imaging problem, typical solutions include: bistatic SAR forward-looking imaging method, single-pulse forward-looking imaging method, real-aperture deconvolution forward-looking imaging method, etc., among which:

1.双基地SAR前视成像方法。是通过双基地SAR系统进行,该系统是指将发射机和接收机分别安装在不同平台上的合成孔径雷达,其发射机和接收机可以有不同的空间位置和运动速度。发射机向观测区域发射线性调频信号;接收机接收地面回波信号并进行成像处理。双基地SAR系统由于其特殊的接收方式,只有在某些特定的模式下,才能实现前视成像,如发射机和接收机有各自独立的飞行轨迹,不能重合,目标点在接收机航迹线沿地面的投影线上;运动误差会极大地影响双基地SAR的前视成像结果,必须进行运动补偿,但是,双基地SAR前视成像的运动补偿分析复杂,相应的补偿技术和方案实施难度很大;现有的算法中,对双基地SAR前视成像结果的几何校正是不完善的,对几何变形的类型和变形量没有完整的理论分析;由于接收机和发射机置于不同的平台上,导致收发分置。因此,双基地SAR前视成像面临着一系列收发系统同步问题,包括时间同步、空间同步和频率同步。1. Bistatic SAR forward-looking imaging method. It is carried out through the bistatic SAR system. This system refers to the synthetic aperture radar with the transmitter and receiver installed on different platforms. The transmitter and receiver can have different spatial positions and movement speeds. The transmitter transmits the chirp signal to the observation area; the receiver receives the ground echo signal and performs imaging processing. Due to its special receiving mode, the bistatic SAR system can only achieve forward-looking imaging in certain specific modes. For example, the transmitter and receiver have their own independent flight paths and cannot overlap. The target point is on the track of the receiver. Along the projection line on the ground; motion errors will greatly affect the forward-looking imaging results of bistatic SAR, and motion compensation must be performed. However, the analysis of motion compensation for bistatic SAR forward-looking imaging is complicated, and the corresponding compensation techniques and schemes are very difficult to implement. Large; in the existing algorithms, the geometric correction of the bistatic SAR forward-looking imaging results is not perfect, and there is no complete theoretical analysis of the type and amount of geometric deformation; since the receiver and the transmitter are placed on different platforms , leading to the separation of transceivers. Therefore, bistatic SAR forward-looking imaging faces a series of synchronization problems of transceiver systems, including time synchronization, space synchronization and frequency synchronization.

2.单脉冲前视成像方法。单脉冲成像的基本思想是利用足够高的距离分辨率分辨出目标上的主要散射体,然后利用单脉冲测角技术获得散射点偏离波束中心的角度,进而用于目标定位。尽管单脉冲测角在理论上具有很高的测量精度,但是在实际应用中,往往存在以下的局限性:在复杂形状目标相对雷达运动时,会引起目标视在中心与目标实际中心的偏离,产生角闪烁现象,制约了成像质量;单脉冲前视成像技术无法对同一距离单元内的不同散射中心分别测角,只能得到等效散射点的位置,降低了测角精度;当同一波束内存在多个目标时,测角精度会急剧下降甚至无法准确检测出目标的位置,特别是当某一距离单元内的波束方位范围中存在两个或多个能量相似的目标时,测角精度尤为低下;单脉冲前视成像中,每个测角坐标平面通常都要采用两个独立的接收支路,即方位平面内的两个支路和俯仰平面内的两个支路,系统复杂。2. Single-pulse forward-looking imaging method. The basic idea of monopulse imaging is to use sufficiently high distance resolution to distinguish the main scatterers on the target, and then use monopulse goniometric technology to obtain the angle of the scattering point away from the center of the beam, and then use it for target positioning. Although monopulse angle measurement has high measurement accuracy in theory, in practical applications, there are often the following limitations: when a complex-shaped target moves relative to the radar, it will cause the deviation between the apparent center of the target and the actual center of the target, Angular flicker phenomenon occurs, which restricts the imaging quality; the single-pulse forward-looking imaging technology cannot measure the angles of different scattering centers in the same range unit, and can only obtain the positions of equivalent scattering points, which reduces the accuracy of angle measurement; when the same beam memory When there are many targets, the angle measurement accuracy will drop sharply and even the position of the target cannot be detected accurately, especially when there are two or more targets with similar energy in the beam azimuth range within a certain distance unit, the angle measurement accuracy is especially Low: In monopulse forward-looking imaging, two independent receiving branches are usually used for each angle measurement coordinate plane, that is, two branches in the azimuth plane and two branches in the elevation plane, and the system is complex.

3.实孔径解卷积前视成像方法。是将雷达传感器输出的回波信号在方位域视为发射信号与目标角度信息的卷积,在距离域视为发射信号与目标距离向信息的卷积,因此理论上可以通过解卷积的方法得到目标的准确位置信息。这种方法操作简单,无需进行运动补偿,系统计算分析难度小。但是,在解卷积过程中也会存在一定的问题:单通道解卷积容易产生病态解,且算法要求较高的信噪比,当信噪比小于30dB时,目标分辨效果较差;为了减小病态效应的影响,Berenstein等人发展了多通道解卷积技术,用于线性移不变系统的信息重建,可使部分解卷积问题转化为良态,但是并非所有的卷积器集合满足强互质条件,当多通道不能满足强互质条件时,解卷积后信噪比仍会大大降低,因此,多通道解卷积技术的使用也存在很大的局限性。3. Real-aperture deconvolution forward-looking imaging method. It regards the echo signal output by the radar sensor as the convolution of the transmitted signal and the target angle information in the azimuth domain, and as the convolution of the transmitted signal and the target range information in the distance domain, so in theory it can be deconvolution method Accurate location information of the target is obtained. This method is simple to operate, does not require motion compensation, and has little difficulty in system calculation and analysis. However, there are also certain problems in the deconvolution process: single-channel deconvolution is prone to produce ill-conditioned solutions, and the algorithm requires a high signal-to-noise ratio. When the signal-to-noise ratio is less than 30dB, the target resolution effect is poor; To reduce the influence of ill-conditioned effects, Berenstein et al. developed multi-channel deconvolution technology for information reconstruction of linear shift invariant systems, which can transform part of the deconvolution problem into a good state, but not all convolution sets Satisfying the strong coprime condition, when the multi-channel cannot satisfy the strong coprime condition, the signal-to-noise ratio will still be greatly reduced after deconvolution. Therefore, the use of multi-channel deconvolution technology also has great limitations.

发明内容 Contents of the invention

本发明的目的在于针对上述已有的前视成像问题的不足,提出了一种基于子空间投影的实孔径前视成像方法,以实现机载雷达前视高分辨成像,降低噪声干扰,提高主瓣内邻近目标的分辨精度。The purpose of the present invention is to address the shortcomings of the above-mentioned existing forward-looking imaging problems, and propose a real-aperture forward-looking imaging method based on subspace projection, so as to realize airborne radar forward-looking high-resolution imaging, reduce noise interference, and improve main Resolution accuracy of nearby targets within the lobe.

本发明的技术方案是:首先对地面监视区域进行顺序重叠扫描,获取雷达回波数据;然后提取回波数据的强度矢量;最后利用一种基于子空间投影的阵列高分辨方法对回波强度矢量进行处理,实现机载雷达前视高分辨成像,其具体步骤包括如下:The technical scheme of the present invention is as follows: firstly, sequential overlapping scanning is performed on the ground monitoring area to obtain radar echo data; then the intensity vector of the echo data is extracted; finally, an array high-resolution method based on subspace projection is used to analyze the echo intensity vector Processing is carried out to realize airborne radar forward-looking high-resolution imaging, and its specific steps include the following:

(1)通过雷达波束的等间距发射,对地面监视区域进行顺序重叠扫描,获取雷达回波数据Y;(1) Sequential overlapping scanning of the ground surveillance area is carried out by transmitting radar beams at equal intervals to obtain radar echo data Y;

(2)对回波数据Y进行取模运算,提取其强度矢量X:(2) Perform a modulo operation on the echo data Y to extract its intensity vector X:

X=|Y(k)|,X=|Y(k)|,

其中,|·|表示取模运算,k=1,2,...,K,K表示回波数据的长度;Wherein, |·| represents the modulus operation, k=1, 2, ..., K, K represents the length of the echo data;

(3)求取回波强度矢量X的自相关矩阵RX(3) Obtain the autocorrelation matrix R X of the echo intensity vector X:

RX=E[XXH],R X =E[XX H ],

其中,X表示回波强度矢量,(·)H表示共轭转置,E[·]表示期望值;Among them, X represents the echo intensity vector, (·) H represents the conjugate transpose, E[·] represents the expected value;

(4)对自相关矩阵RX进行特征分解,将其分解为特征值和特征向量的乘累加形式:(4) Carry out eigendecomposition on the autocorrelation matrix R X , and decompose it into the form of multiplication and accumulation of eigenvalues and eigenvectors:

RR Xx == ΣΣ jj == 11 NN λλ jj vv jj vv jj Hh ,,

其中,λj表示第j个特征值,vj表示第j个特征向量,(·)H表示共轭转置,j=1,2,...,N,N表示特征值的数目;Wherein, λ j represents the j eigenvalue, v j represents the j eigenvector, ( ) H represents the conjugate transpose, j=1, 2, ..., N, N represents the number of eigenvalues;

(5)将特征值λj按升序排列λ1=λ2=...=λN-p≤λN-p+1≤...≤λN,并相应地调整特征向量顺序为:v1,v2,...,vN-p,vN-p+1,...,vN,用前N-P个小特征值对应的特征向量构成噪声子空间EN(5) Arrange the eigenvalues λ j in ascending order λ 12 =...=λ Np ≤λ N-p+1 ≤...≤λ N , and adjust the order of the eigenvectors accordingly: v 1 , v 2 ,...,v Np , v N-p+1 ,...,v N , use the eigenvectors corresponding to the first NP small eigenvalues to form the noise subspace E N :

EN=[v1,v2,...,vN-p],E N = [v 1 , v 2 , . . . , v Np ],

其中,p表示信号的数目,N表示特征值的数目;Among them, p represents the number of signals, and N represents the number of eigenvalues;

(6)定义方向图搜索矢量集合a:(6) Define the direction map search vector set a:

a=[ai],a=[a i ],

其中,ai表示第i个方向图搜索矢量,i=1,2,...,2M,M表示方向图搜索矢量的长度;Wherein, a i represents the i-th pattern search vector, i=1, 2, ..., 2M, and M represents the length of the pattern search vector;

aa ii == [[ sinsin [[ nno (( MτMτ ++ δδ ii )) ]] nno (( MτMτ ++ δδ ii )) ,, sinsin [[ (( nno (( (( Mm -- 11 )) ττ ++ δδ ii )) ]] nno [[ (( Mm -- 11 )) ττ ++ δδ ii ]] ,, .. .. .. ,, sinsin [[ nno (( (( -- Mm )) ττ ++ δδ ii )) ]] nno [[ (( -- Mm )) ττ ++ δδ ii ]] ]] TT ,,

其中,(·)T表示转置,δi表示第i个方向图搜索矢量的位移,n为一个固定的参数,控制方向图的主瓣宽度,τ代表了扫描密集程度,

Figure BDA0000144833440000041
b_width表示主瓣宽度,d为一个变化的参数;Among them, ( ) T represents the transpose, δ i represents the displacement of the i-th pattern search vector, n is a fixed parameter, which controls the main lobe width of the pattern, and τ represents the scanning density,
Figure BDA0000144833440000041
b_width represents the width of the main lobe, and d is a variable parameter;

(7)将第i个方向图搜索矢量ai投影到噪声子空间EN上,得到搜索矢量在噪声子空间上的投影:(7) Project the i-th direction map search vector a i onto the noise subspace E N to obtain the projection of the search vector on the noise subspace:

EE. NN aa ii == [[ ΣΣ jj == 11 NN -- pp vv jj vv jj Hh ]] aa ii ,,

其中,vj表示小特征值对应的特征矢量,(·)H表示共轭转置,p表示信号的数目,N表示特征值的数目;Among them, v j represents the eigenvector corresponding to the small eigenvalue, ( ) H represents the conjugate transpose, p represents the number of signals, and N represents the number of eigenvalues;

(8)计算空间谱函数:(8) Calculate the spatial spectral function:

PP (( ii )) == 11 // || || EE. NN aa ii || || 22 22 ,,

其中,EN表示噪声子空间,ai表示搜索矢量,表示二范数的平方;where E N represents the noise subspace, a i represents the search vector, Represents the square of the two-norm;

(9)根据空间谱函数峰值的数目确定信号的个数,以分辨主瓣内的邻近目标,完成沿航迹线方向目标的检测与识别,实现前视高分辨成像。(9) Determine the number of signals according to the number of peaks of the spatial spectrum function to distinguish adjacent targets in the main lobe, complete the detection and identification of targets along the track line, and realize forward-looking high-resolution imaging.

本发明与现有技术相比,具有以下优点:Compared with the prior art, the present invention has the following advantages:

(1)本发明通过对回波数据的强度提取矢量进行成像处理,不会产生角闪烁现象,能对同一主瓣内的多个目标进行分离,甚至可以检测出同一波束内能量相似的两个目标,有效地提高了检测精度和成像质量;(1) The present invention performs imaging processing on the intensity extraction vector of the echo data, which does not produce angular flicker phenomenon, can separate multiple targets in the same main lobe, and can even detect two objects with similar energy in the same beam. target, effectively improving the detection accuracy and imaging quality;

(2)本发明仅需要一个通道接收回波数据,利于系统实现;(2) The present invention only needs one channel to receive echo data, which is beneficial to system realization;

(3)本发明通过构造噪声子空间的方法,可以减缓噪声对信号的影响,且不会产生病态解。(3) The present invention can alleviate the influence of noise on the signal through the method of constructing the noise subspace, and will not generate ill-conditioned solutions.

附图说明 Description of drawings

图1是本发明的前视成像的总流程图;Fig. 1 is the general flow chart of the forward vision imaging of the present invention;

图2是本发明中的顺序重叠扫描示意图;Fig. 2 is a schematic diagram of sequential overlapping scanning in the present invention;

图3是本发明的前视成像结果;Fig. 3 is the forward vision imaging result of the present invention;

图4是本发明用四个旁瓣方向图扫描后的目标分辨概率;Fig. 4 is the target resolution probability after scanning with four side lobe patterns in the present invention;

图5是本发明用无旁瓣方向图扫描后的目标分辨概率;Fig. 5 is the target resolution probability after scanning with no sidelobe pattern in the present invention;

图6是本发明在目标间隔1/4主瓣宽度下的分辨概率与信噪比的关系图;Fig. 6 is the relationship diagram of the resolution probability and the signal-to-noise ratio under the target interval 1/4 main lobe width of the present invention;

图7是本发明在信噪比10dB时扫描间隔与最小目标间隔的关系图。FIG. 7 is a graph showing the relationship between the scanning interval and the minimum target interval when the signal-to-noise ratio is 10 dB in the present invention.

具体实施方式 Detailed ways

参照图1,本发明的实施步骤如下:With reference to Fig. 1, the implementation steps of the present invention are as follows:

步骤1:通过雷达波束的等间距发射,对地面监视区域进行顺序重叠扫描,获取雷达回波数据Y;Step 1: Sequential overlapping scanning of the ground monitoring area is carried out by transmitting radar beams at equal intervals to obtain radar echo data Y;

参照图2,本步骤机载雷达对地面监视区域进行顺序重叠扫描,就是将雷达回波数据视为天线波束与目标信息的卷积,通过等间距发射雷达波束,获取回波数据Y。Referring to Figure 2, in this step, the airborne radar sequentially overlaps and scans the ground surveillance area, that is, the radar echo data is regarded as the convolution of the antenna beam and the target information, and the echo data Y is obtained by emitting radar beams at equal intervals.

步骤2:对回波数据Y进行取模运算,提取其强度矢量X:Step 2: Perform a modulo operation on the echo data Y to extract its intensity vector X:

X=|Y(k)|,                                                      1)X=|Y(k)|, 1)

其中,|·|表示取模运算,k=1,2,...,K,K表示回波数据的长度。Wherein, |·| represents a modulo operation, k=1, 2, . . . , K, K represents the length of the echo data.

将强度矢量X表示为信号幅度值和方向图矢量的乘累加形式:Express the intensity vector X as a multiply-accumulate form of the signal amplitude value and the pattern vector:

Xx == ΣΣ tt == 11 pp sthe s tt aa tt ++ NN ,, -- -- -- 22 ))

其中,N表示噪声矢量,st表示第t个信号的幅度值,at表示第t个信号对应的方向图矢量,t=1,...,p,p表示信号数目。Wherein, N represents the noise vector, s t represents the amplitude value of the t-th signal, at represents the pattern vector corresponding to the t-th signal, t=1, ..., p, p represents the number of signals.

步骤3:求取回波强度矢量X的自相关矩阵RXStep 3: Obtain the autocorrelation matrix R X of the echo intensity vector X:

RX=E[XXH],                                                     3)R x =E[XX H ], 3)

其中,X表示回波强度矢量,(·)H表示共轭转置,E[·]表示期望值。Among them, X represents the echo intensity vector, (·) H represents the conjugate transpose, and E[·] represents the expected value.

步骤4:对自相关矩阵RX进行特征分解,将其分解为特征值和特征向量的乘累加形式:Step 4: Carry out eigendecomposition on the autocorrelation matrix R X , and decompose it into the form of multiplication and accumulation of eigenvalues and eigenvectors:

RR Xx == ΣΣ jj == 11 NN λλ jj vv jj vv jj Hh ,, -- -- -- 44 ))

其中,λj表示第j个特征值,vj表示第j个特征向量,(·)H表示共轭转置,j=1,2,...,N,N表示特征值的数目。Among them, λ j represents the jth eigenvalue, v j represents the jth eigenvector, (·) H represents the conjugate transpose, j=1, 2, ..., N, N represents the number of eigenvalues.

步骤5:将特征值λj按升序排列λ1=λ2=...=λN-p≤λN-p+1≤...≤λN,并相应地调整特征向量顺序为:v1,v2,...,vN-p,vN-p+1,...,vN,用前N-P个小特征值对应的特征向量构成噪声子空间ENStep 5: Arrange the eigenvalues λ j in ascending order λ 12 =...=λ Np ≤λ N-p+1 ≤...≤λ N , and adjust the order of the eigenvectors accordingly: v 1 , v 2 ,...,v Np , v N-p+1 ,...,v N , use the eigenvectors corresponding to the first NP small eigenvalues to form the noise subspace E N :

EN=[v1,v2,...,vN-p],                                         5)E N = [v 1 , v 2 , . . . , v Np ], 5)

其中,p表示信号的数目,N表示特征值的数目。Among them, p represents the number of signals, and N represents the number of eigenvalues.

步骤6:定义方向图搜索矢量集合a:Step 6: Define the direction map search vector set a:

a=[ai],                                                         6)a=[a i ], 6)

其中,ai表示第i个方向图搜索矢量,i=1,2,...,2M,M表示方向图搜索矢量的长度;Wherein, a i represents the i-th pattern search vector, i=1, 2, ..., 2M, and M represents the length of the pattern search vector;

aa ii == [[ sinsin [[ nno (( MτMτ ++ δδ ii )) ]] nno (( MτMτ ++ δδ ii )) ,, sinsin [[ (( nno (( (( Mm -- 11 )) ττ ++ δδ ii )) ]] nno [[ (( Mm -- 11 )) ττ ++ δδ ii ]] ,, .. .. .. ,, sinsin [[ nno (( (( -- Mm )) ττ ++ δδ ii )) ]] nno [[ (( -- Mm )) ττ ++ δδ ii ]] ]] TT ,, -- -- -- 77 ))

其中,(·)T表示转置,δi表示第i个方向图搜索矢量的位移,n为一个固定的参数,控制方向图的主瓣宽度,τ代表了扫描密集程度,

Figure BDA0000144833440000062
b_width表示主瓣宽度,d为一个变化的参数。Among them, ( ) T represents the transpose, δ i represents the displacement of the i-th pattern search vector, n is a fixed parameter, which controls the main lobe width of the pattern, and τ represents the scanning density,
Figure BDA0000144833440000062
b_width represents the width of the main lobe, and d is a variable parameter.

步骤7:将第i个方向图搜索矢量ai投影到噪声子空间EN上,得到搜索矢量在噪声子空间上的投影:Step 7: Project the i-th direction map search vector a i onto the noise subspace E N to get the projection of the search vector on the noise subspace:

EE. NN aa ii == [[ ΣΣ jj == 11 NN -- pp vv jj vv jj Hh ]] aa ii ,, -- -- -- 88 ))

其中,vj表示小特征值对应的特征矢量,(·)H表示共轭转置,p表示信号的数目,N表示特征值的数目。Among them, v j represents the eigenvector corresponding to the small eigenvalue, ( ) H represents the conjugate transpose, p represents the number of signals, and N represents the number of eigenvalues.

步骤8:计算空间谱函数:Step 8: Calculate the spatial spectral function:

PP (( ii )) == 11 // || || EE. NN aa ii || || 22 22 ,, -- -- -- 88 ))

其中,EN表示噪声子空间,ai表示i个方向图搜索矢量,表示二范数的平方。where E N represents the noise subspace, a i represents i pattern search vectors, Represents the square of the binorm.

步骤9:跟据空间谱函数峰值的数目确定信号的个数,以分辨主瓣内的邻近目标,完成沿航迹线方向目标的检测与识别,实现前视高分辨成像。Step 9: Determine the number of signals according to the number of peaks of the spatial spectrum function to distinguish adjacent targets in the main lobe, complete the detection and identification of targets along the track line, and realize forward-looking high-resolution imaging.

由于信号子空间和噪声子空间的正交性,信号对应的方向图矢量ai在噪声子空间EN上的投影最小,形成空间谱函数P(i)的峰值,因此空间谱函数峰值的数目即为信号的个数,以此完成沿航迹线方向目标的检测与识别,实现前视高分辨成像。Due to the orthogonality of the signal subspace and the noise subspace, the projection of the direction diagram vector a i corresponding to the signal on the noise subspace E N is the smallest, forming the peak of the spatial spectral function P(i), so the number of spatial spectral function peaks That is, the number of signals, so as to complete the detection and identification of targets along the flight path, and realize forward-looking high-resolution imaging.

本发明的效果可通过以下仿真进一步说明:Effect of the present invention can be further illustrated by following simulation:

仿真1,验证本发明所提方法的成像结果。Simulation 1, to verify the imaging results of the method proposed in the present invention.

在方向图间隔1/4主瓣宽度下顺序重叠扫描地面点目标,两个点目标的间距为1/4主瓣宽度,信噪比为10dB,快拍500次,前视成像结果如图3所示。Sequentially overlap and scan the ground point targets under the pattern interval of 1/4 the main lobe width, the distance between the two point targets is 1/4 the main lobe width, the signal-to-noise ratio is 10dB, and snapshots are taken 500 times. The forward-looking imaging results are shown in Figure 3 shown.

观察图3可以发现,本发明所提方法可以分辨主瓣内邻近的两个目标。这是因为基于子空间投影的阵列高分辨成像方法通过构造噪声子空间的方式,能够减小噪声的影响,提高目标的检测精度。Observing FIG. 3, it can be found that the method proposed in the present invention can distinguish two adjacent targets in the main lobe. This is because the array high-resolution imaging method based on subspace projection can reduce the influence of noise and improve the detection accuracy of the target by constructing the noise subspace.

仿真2,验证旁瓣对目标分辨概率的影响。Simulation 2, to verify the impact of side lobes on target resolution probability.

在方向图间隔1/4主瓣宽度下顺序重叠扫描地面点目标,两个点目标的间距为1/4主瓣宽度,信噪比为10dB,快拍500次,并进行Monte Carlo实验200次,分别得到用四个旁瓣方向图扫描后的目标分辨概率如图4所示,和用无旁瓣方向图扫描后的目标分辨概率如图5所示。Sequentially overlap and scan the ground point targets at a pattern interval of 1/4 the main lobe width, the distance between two point targets is 1/4 the main lobe width, the signal-to-noise ratio is 10dB, take 500 snapshots, and conduct Monte Carlo experiments 200 times , the target resolution probabilities obtained after scanning with four sidelobe patterns are shown in Fig. 4, and the target resolution probabilities after scanning with no sidelobe pattern are shown in Fig. 5.

观察图4和图5可以发现,旁瓣的数量,对目标分辨概率的影响很小。这是因为,旁瓣的能量很小,在实际应用中,可以忽略不计。Observing Figure 4 and Figure 5, it can be found that the number of side lobes has little effect on the target resolution probability. This is because the energy of the side lobes is very small and can be ignored in practical applications.

仿真3,验证信噪比对目标分辨概率的影响。Simulation 3, to verify the influence of signal-to-noise ratio on target resolution probability.

在方向图间隔1/4主瓣宽度下顺序重叠扫描地面点目标,两个点目标的间距为1/4主瓣宽度,快拍500次,并进行Monte Carlo实验500次,得到分辨概率与信噪比的关系如图6所示。The point targets on the ground are overlapped and scanned sequentially under the interval of 1/4 of the main lobe width of the pattern, the distance between two point targets is 1/4 of the main lobe width, snapshots are taken 500 times, and Monte Carlo experiments are carried out 500 times, and the resolution probability and signal are obtained. The relationship between the noise ratio is shown in Figure 6.

观察图6可以发现,信噪比越小,目标的分辨概率越低。这是因为低信噪比下,信号会湮没在噪声中,无法求得正确的信号子空间和噪声子空间,致使目标分辨概率降低。Observing Figure 6, it can be found that the smaller the signal-to-noise ratio, the lower the target resolution probability. This is because at a low SNR, the signal will be buried in the noise, and the correct signal subspace and noise subspace cannot be obtained, resulting in a decrease in the target resolution probability.

仿真4,验证不同扫描间隔下可分辨的最小目标间隔。Simulation 4, to verify the resolvable minimum target interval under different scan intervals.

在分辨概率的门限值为90%,信噪为10dB的条件下,快拍500次,Monte Carlo实验100次,得到扫描间隔与最小目标间隔的关系如图7所示。Under the condition that the threshold of resolution probability is 90% and the signal-to-noise is 10dB, 500 snapshots and 100 Monte Carlo experiments are performed, and the relationship between the scan interval and the minimum target interval is shown in Figure 7.

观察图7可以发现,在信噪比为10dB时,目标间隔的极限值为1/5主瓣宽度,即只有当目标间隔大于等于1/5主瓣宽度时,才能进行前视高分辨成像。Observing Figure 7, it can be found that when the signal-to-noise ratio is 10dB, the limit value of the target interval is 1/5 of the main lobe width, that is, only when the target interval is greater than or equal to 1/5 of the main lobe width, forward-looking high-resolution imaging can be performed.

Claims (1)

1. the real aperture forward sight formation method based on subspace projection comprises the steps:
(1) through the equidistant emission of radar beam, the order overlapping scan is carried out in the surface surveillance zone, obtains the radar return data Y;
(2) echo data Y is carried out modulo operation, extracts its strength vector X:
X=|Y(k)|,
Wherein, || the expression modulo operation, k=1,2 ..., K, K represent the length of echo data;
(3) ask for the autocorrelation matrix R of echo strength vector X X:
R X=E[XX H],
Wherein, X representes echo strength vector, () HThe expression conjugate transpose, E [] representes expectation value;
(4) to autocorrelation matrix R XCarry out feature decomposition, it be decomposed into the multiply accumulating form of eigenwert and proper vector:
R X = Σ j = 1 N λ j v j v j H ,
Wherein, λ jRepresent j eigenwert, v jRepresent j proper vector, () HThe expression conjugate transpose, j=1,2 ..., N, the number of N representation feature value;
(5) with eigenvalue jArrange λ by ascending order 12=...=λ N-p≤λ N-p+1≤...≤λ N, and correspondingly adjust proper vector and be in proper order: v 1, v 2..., v N-p, v N-p+1..., v N, constitute noise subspace E with preceding N-P little eigenwert characteristic of correspondence vector N:
E N=[v 1,v 2,...,v N-p],
Wherein, the number of p expression signal, the number of N representation feature value;
(6) definition directional diagram search vector set a:
a=[a i],
Wherein, a iRepresent i directional diagram search vector, i=1,2 ..., 2M, M represent the length of directional diagram search vector;
a i = [ sin [ n ( Mτ + δ i ) ] n ( Mτ + δ i ) , sin [ ( n ( ( M - 1 ) τ + δ i ) ] n [ ( M - 1 ) τ + δ i ] , . . . , sin [ n ( ( - M ) τ + δ i ) ] n [ ( - M ) τ + δ i ] ] T ,
Wherein, () TThe expression transposition, δ iRepresent the displacement of i directional diagram search vector, n is a fixing parameter, the main lobe width of control directional diagram, and τ has represented the scanning dense degree,
Figure FDA0000144833430000022
B_width representes main lobe width, and d is the parameter of a variation;
(7) with i directional diagram search vector a iProject to noise subspace E NOn, obtain the projection of search vector on noise subspace:
E N a i = [ Σ j = 1 N - p v j v j H ] a i ,
Wherein, v jRepresent little eigenwert characteristic of correspondence vector, () HThe expression conjugate transpose, the number of p expression signal, the number of N representation feature value;
(8) computer memory spectral function:
P ( i ) = 1 / | | E N a i | | 2 2 ,
Wherein, E NThe expression noise subspace, a iThe expression search vector,
Figure FDA0000144833430000025
Represent two norms square;
(9) confirm the number of signal according to the number of spatial spectrum peak of function,, accomplish detection and identification, realize the forward sight high-resolution imaging along track line direction target to differentiate the adjacent objects in the main lobe.
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