CN103278819B - Onboard high-resolution strabismus bunching synthetic aperture radar (SAR) imaging method based on sliding receiving window - Google Patents
Onboard high-resolution strabismus bunching synthetic aperture radar (SAR) imaging method based on sliding receiving window Download PDFInfo
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Abstract
本发明公开了一种基于滑动接收窗的机载高分辨率斜视聚束SAR成像方法,包括以下几个步骤:步骤一:读入原始回波数据及相关成像参数;步骤二:方位向解线性调频处理;步骤三:方位向傅里叶变换处理;步骤四:方位向解线性调频残留相位误差补偿处理;步骤五:距离向傅里叶变换处理;步骤六:一致压缩处理;步骤七:斯托尔特(stolt)插值处理;步骤八:方位向傅里叶逆变换处理;步骤九:几何校正处理;步骤十:距离向傅里叶变换处理;本发明提出了一种基于滑动接收窗的机载高分辨率斜视聚束SAR成像方法,解决了目前基于滑动接收窗技术的机载高分辨率斜视聚束SAR原始回波数据没有成像方法的现状。
The invention discloses an airborne high-resolution squint spotlight SAR imaging method based on a sliding receiving window, which includes the following steps: Step 1: read in the original echo data and related imaging parameters; Frequency modulation processing; step three: azimuth Fourier transform processing; step four: azimuth de-chirp residual phase error compensation processing; step five: range to Fourier transform processing; step six: consistent compression processing; step seven: Si Tolt (stolt) interpolation processing; step eight: azimuth to Fourier inverse transform processing; step nine: geometric correction processing; step ten: distance to Fourier transform processing; the present invention proposes a sliding receiving window based The airborne high-resolution squint spotlight SAR imaging method solves the current situation that there is no imaging method for the original echo data of airborne high-resolution squint spotlight SAR based on sliding receiving window technology.
Description
技术领域technical field
本发明属于信号处理领域,特别涉及一种基于滑动接收窗的机载高分辨率斜视聚束合成孔径雷达合成孔径雷达(Synthetic Aperture Radar,SAR)成像方法。The invention belongs to the field of signal processing, in particular to an airborne high-resolution squint spotlight synthetic aperture radar synthetic aperture radar (Synthetic Aperture Radar, SAR) imaging method based on a sliding receiving window.
背景技术Background technique
SAR是一种工作在微波频段的主动遥感器,克服了光学成像受天气和光照条件限制的缺陷,能全天时、全天候、远距离的进行对地遥感观测,并能够穿透天然植被、人工伪装等,大大提高了雷达的信息捕获能力。因此,SAR已经成为雷达技术的热门研究领域,为越来越多的国家所重视。相比于传统的侧视SAR系统,机载斜视SAR成像在实际应用中具有很高的灵活性和机动性,通过调整天线波束指向,SAR系统可自由灵活地选择观测区域,并且能够快速重访敏感区域,大大提高了SAR的观测能力。此外,随着SAR分辨率的提高,使得SAR目标侦察与识别能力得到显著提升。因此,近些年来,高分辨率斜视成像已经成为一个重要的发展方向。SAR is an active remote sensor that works in the microwave frequency band. It overcomes the limitations of optical imaging due to weather and light conditions. Camouflage, etc., greatly improved the information capture capability of the radar. Therefore, SAR has become a popular research field of radar technology, and more and more countries pay attention to it. Compared with the traditional side-looking SAR system, airborne squint SAR imaging has high flexibility and maneuverability in practical applications. By adjusting the antenna beam pointing, the SAR system can freely and flexibly select the observation area, and can quickly revisit Sensitive areas, greatly improving the observation capabilities of SAR. In addition, with the improvement of SAR resolution, the ability of SAR target reconnaissance and recognition has been significantly improved. Therefore, high-resolution squint imaging has become an important development direction in recent years.
但是,高分辨率大斜视SAR成像也带来了新的技术难点。一方面,随着斜视角度的增大,SAR原始回波方位向与距离向耦合现象更加严重,导致高精度成像更加困难;另一方面,距离徙动量随斜视角的增加以及分辨率的增加而成几何级数增长,导致SAR原始回波数据量的显著增加,加大了数据存储与实时成像的困难。滑动接收窗技术是指通过改变回波窗开启时刻,消除距离徙动中的一次项,即距离走动。滑动接收窗技术能够减小SAR原始回波距离徙动量,进而减小SAR原始回波数据量。但是,滑动接收窗技术调整了回波数据的录取起始时间,观测区域内每一个目标的多普勒历程也随方位向发生了变化,使得传统成像方法不再适用。However, high-resolution high-squint SAR imaging also brings new technical difficulties. On the one hand, as the squint angle increases, the azimuth and range coupling of the original SAR echo becomes more serious, making high-precision imaging more difficult; The geometric progression increases, leading to a significant increase in the amount of SAR original echo data, increasing the difficulty of data storage and real-time imaging. The sliding receiving window technology refers to eliminating the one-time item in the distance migration by changing the opening time of the echo window, that is, the distance walking. The sliding receiving window technology can reduce the distance migration of SAR original echoes, thereby reducing the amount of SAR original echo data. However, the sliding receiving window technology adjusts the start time of echo data acquisition, and the Doppler history of each target in the observation area also changes with the azimuth, making the traditional imaging method no longer applicable.
发明内容Contents of the invention
本发明的目的是为了解决上述问题,基于滑动接收窗技术特点,结合传统波数域成像方法,提出了一种基于滑动接收窗的机载高分辨率斜视聚束SAR成像方法。The purpose of the present invention is to solve the above problems. Based on the technical characteristics of the sliding receiving window and combined with the traditional wavenumber domain imaging method, an airborne high-resolution squint spotlight SAR imaging method based on the sliding receiving window is proposed.
一种基于滑动接收窗的机载高分辨率斜视聚束SAR成像方法,包括以下几个步骤:An airborne high-resolution squint spotlight SAR imaging method based on a sliding receiving window, comprising the following steps:
步骤一:读入原始回波数据及相关成像参数;Step 1: Read in the original echo data and related imaging parameters;
读入基于滑动接收窗的机载高分辨率斜视聚束SAR二维原始回波仿真复数据Sstart以及相应的成像参数,具体包括:方位向采样点数Na,距离向采样点数Nr,信号采样率fs,信号带宽Bw,脉冲宽度τ,调频斜率b,脉冲重复频率PRF,参考斜距Rref,多普勒中心频率fd0,多普勒调频率fr0,卫星速度Pv,等效斜视角信号波长λ,信号载频f0,信号传播速度c;Read in the airborne high-resolution squint spotlight SAR two-dimensional original echo simulation complex data S start and the corresponding imaging parameters based on the sliding receiving window, including: the number of sampling points in azimuth N a , the number of sampling points in range N r , the signal Sampling rate f s , signal bandwidth Bw, pulse width τ, frequency modulation slope b, pulse repetition frequency PRF, reference slope distance R ref , Doppler center frequency fd 0 , Doppler modulation frequency f r0 , satellite velocity P v , etc. Effective oblique angle Signal wavelength λ, signal carrier frequency f 0 , signal propagation speed c;
步骤二:方位向解线性调频处理;Step 2: azimuth dechirp processing;
将二维回波仿真复数据Sstart进行方位向解线性调频处理:首先复数据Sstart同因子H1相乘,得到复数据S1_1;其次对复数据S1_1做方位向傅里叶变换,即沿每个距离向(按列)进行快速傅里叶变化(FFT),得到复数据S1_2;最后将复数据S1_2同因子H2相乘,得到最终方位向解线性调频后的复数据S1;The two-dimensional echo simulation complex data S start is subjected to azimuth dechirp processing: firstly, the complex data S start is multiplied by the factor H 1 to obtain the complex data S 1_1 ; secondly, the complex data S 1_1 is subjected to Fourier transform in azimuth direction, That is, fast Fourier transform (FFT) is performed along each distance direction (by column) to obtain complex data S 1_2 ; finally, the complex data S 1_2 is multiplied by the factor H 2 to obtain the complex data after de-chirping the final azimuth direction S 1 ;
步骤三:方位向傅里叶变换处理;Step 3: Azimuth to Fourier transform processing;
将步骤二得到的复数据S1沿每个距离向(按列)进行快速傅里叶变换(FFT),得到方位向频谱复数据S2;Perform fast Fourier transform (FFT) on the complex data S 1 obtained in step 2 along each distance direction (by column) to obtain complex data S 2 in the azimuth direction spectrum;
步骤四:方位向解线性调频残留相位误差补偿处理;Step 4: Azimuth de-chirp residual phase error compensation processing;
将步骤三得到的复数据S2同对应方位时刻的方位向解线性调频残留相位误差补偿因子Ω1相乘,得到补偿后的复数据S3;Multiply the complex data S 2 obtained in step 3 with the azimuth dechirp residual phase error compensation factor Ω 1 at the corresponding azimuth moment to obtain the compensated complex data S 3 ;
步骤五:距离向傅里叶变换处理;Step five: distance to Fourier transform processing;
将步骤四得到的复数据S3沿每个方位时刻(按行)进行快速傅里叶变换(FFT),得到二维频谱复数据S4;Perform fast Fourier transform (FFT) on the complex data S 3 obtained in step 4 along each azimuth moment (by row) to obtain two-dimensional spectrum complex data S 4 ;
步骤六:一致压缩处理;Step 6: consistent compression processing;
将步骤五得到的复数据S4同对应的一致压缩因子Ω2相乘,得到粗聚焦复数据S5;Multiply the complex data S 4 obtained in step 5 with the corresponding consistent compression factor Ω 2 to obtain the coarse-focus complex data S 5 ;
步骤七:斯托尔特(stolt)插值处理;Step 7: Stolt (stolt) interpolation processing;
对于步骤六得到的复数据S5,利用辛格(sinc)插值法进行stolt插值处理,得到由二维频域映射到二维波数域的复数据S6;For the complex data S 5 obtained in step 6, Singer (sinc) interpolation method is used to perform stolt interpolation processing to obtain complex data S 6 mapped from the two-dimensional frequency domain to the two-dimensional wavenumber domain;
步骤八:方位向傅里叶逆变换处理;Step 8: Azimuth inverse Fourier transform processing;
将步骤七得到的复数据S6沿每个距离向(按列)进行快速傅里叶逆变换(IFFT),得到方位时域距离波数域复数据S7;Perform inverse fast Fourier transform (IFFT) on the complex data S 6 obtained in step 7 along each distance direction (column), to obtain the complex data S 7 in the azimuth time domain distance wavenumber domain;
步骤九:几何校正处理;Step 9: Geometric correction processing;
将步骤八得到的复数据S7同几何校正因子Ω3相乘,得到经几何校正后的复数据S8;Multiply the complex data S 7 obtained in step 8 with the geometric correction factor Ω 3 to obtain complex data S 8 after geometric correction;
步骤十:距离向傅里叶变换处理;Step ten: distance to Fourier transform processing;
将步骤九得到的复数据S9沿每个方位时刻(按行)进行快速傅里叶逆变换(IFFT),得到最终的成像结果Send;Perform inverse fast Fourier transform (IFFT) on the complex data S 9 obtained in step 9 along each azimuth moment (by row) to obtain the final imaging result S end ;
本发明优点在于:The present invention has the advantage that:
(1)本发明提出了一种基于滑动接收窗的机载高分辨率斜视聚束SAR成像方法,解决了目前基于滑动接收窗技术的机载高分辨率斜视聚束SAR原始回波数据没有成像方法的现状。(1) The present invention proposes an airborne high-resolution squint spotlight SAR imaging method based on a sliding receiving window, which solves the problem that the original echo data of airborne high-resolution squint spotlight SAR based on sliding receiving window technology is not imaged The current state of the method.
(2)本发明提出了一种基于滑动接收窗的机载高分辨率斜视聚束SAR成像方法,具有高精度聚焦成像的特点。由于本发明提出的成像方法是一种改进的波数域成像方法,而波数域成像方法的优势是,只要满足速度恒定这一条件(机载SAR恰好满足这一条件),就能够实现高精度聚焦。因此,利用本发明能够实现场景高精度聚焦成像。(2) The present invention proposes an airborne high-resolution squint spotlight SAR imaging method based on a sliding receiving window, which has the characteristics of high-precision focused imaging. Since the imaging method proposed in the present invention is an improved wavenumber domain imaging method, the advantage of the wavenumber domain imaging method is that it can achieve high-precision focusing as long as the condition of constant speed is satisfied (airborne SAR just meets this condition). . Therefore, the present invention can realize high-precision focused imaging of the scene.
(3)本发明提出了一种基于滑动接收窗的机载高分辨率斜视聚束SAR成像方法,具有适用性强的特点。一方面,由于本发明提出的成像方法是一种改进的波数域成像方法,而波数域成像方法不受斜视角度的限制,因此,在斜视角度很大的条件下,本发明同样能实现场景的精确聚焦,得到高质量的SAR图像。另一方面,本发明能够实现0.1m超高分辨率成像,并得到精确聚焦,因此,本发明适用于目前各种分辨率的成像要求。(3) The present invention proposes an airborne high-resolution squint spotlight SAR imaging method based on a sliding receiving window, which has the characteristics of strong applicability. On the one hand, since the imaging method proposed by the present invention is an improved wavenumber domain imaging method, and the wavenumber domain imaging method is not limited by the angle of the squint, the present invention can also realize the image of the scene when the angle of the squint is large. Precise focus to get high-quality SAR images. On the other hand, the present invention can realize 0.1m ultra-high resolution imaging and obtain precise focus, therefore, the present invention is applicable to current imaging requirements of various resolutions.
附图说明Description of drawings
图1是本发明提出的一种基于滑动接收窗的机载高分辨率斜视聚束SAR成像方法流程图;Fig. 1 is a kind of airborne high-resolution squint spotlight SAR imaging method flow chart based on the sliding receiving window proposed by the present invention;
图2是实施例仿真场景示意图;Fig. 2 is a schematic diagram of an embodiment simulation scene;
图3是实施例成像结果;Fig. 3 is embodiment imaging result;
图4是实施例左上点目标剖面图;Fig. 4 is the upper left point target sectional view of the embodiment;
图5是实施例中间点目标剖面图;Fig. 5 is the cross-sectional view of the middle point target of the embodiment;
图6是实施例右下点目标剖面图。Fig. 6 is a sectional view of the lower right point target of the embodiment.
具体实施方式Detailed ways
下面将结合附图和实施例对本发明作进一步的详细说明。The present invention will be further described in detail with reference to the accompanying drawings and embodiments.
本发明提出一种基于滑动接收窗的机载分辨率斜视聚束SAR成像方法,处理的对象是基于滑动接收窗的机载高分辨率斜视聚束SAR原始回波数据,得到的结果是一幅高分辨率斜视图像。The invention proposes an airborne resolution squint spotlight SAR imaging method based on a sliding receiving window. The processing object is the original echo data of the airborne high resolution squint spotlight SAR based on a sliding receiving window, and the obtained result is a High resolution squint images.
滑动接收窗是指SAR在接收回波时,回波接收窗开启时刻随方位时刻而改变,从而减小目标的距离徙动,或者说消除目标的距离走动(距离徙动中的线性部分)。采用滑动接收窗的SAR系统在工作中各方位时刻回波窗开启时刻T'(i)为:The sliding receiving window means that when the SAR receives the echo, the opening time of the echo receiving window changes with the azimuth time, thereby reducing the range migration of the target, or eliminating the range walking of the target (the linear part in the range migration). The opening time T'(i) of the echo window at each azimuth time of the SAR system using the sliding receiving window is:
其中,T0是相同条件下传统SAR系统固定回波窗开启时刻,fd0是指多普勒中心频率,λ指信号波长,c指信号传播速度,t(i)是指方位时刻,且,i=0,1,2,…,Na-1。滑动接收窗技术减小了回波的距离徙动量,进而减小了回波数据量,缓解了数据存储和实时成像的压力。Among them, T 0 is the opening time of the traditional SAR system fixed echo window under the same conditions, fd 0 refers to the Doppler center frequency, λ refers to the signal wavelength, c refers to the signal propagation speed, t(i) refers to the azimuth time, and , i=0, 1, 2, . . . , N a -1. The sliding receiving window technology reduces the distance migration of the echo, thereby reducing the amount of echo data and relieving the pressure of data storage and real-time imaging.
本发明是一种基于滑动接收窗的机载高分辨率斜视聚束SAR成像方法,具体流程如图1所示,包括以下步骤:The present invention is an airborne high-resolution squint spotlight SAR imaging method based on a sliding receiving window. The specific process is shown in Figure 1, comprising the following steps:
步骤一:读入基于滑动接收窗的机载高分辨率斜视聚束SAR二维原始回波复数据Sstart以及相应的成像参数。其中,Sstart是一个二维复数组,大小为Na×Nr,而成像参数具体包括:方位向采样点数Na、距离向采样点数Nr、信号采样率fs、信号带宽Bw、调频斜率b、脉冲重复频率PRF、参考斜距Rref、多普勒中心频率fd0、多普勒调频率fr0、卫星速度Pv、等效斜视角、信号波长λ、信号载频f0、信号传播速度c;Step 1: Read in the airborne high-resolution squint spotlight SAR two-dimensional original echo complex data S start and the corresponding imaging parameters based on the sliding receiving window. Among them, S start is a two-dimensional complex array with a size of N a ×N r , and the imaging parameters specifically include: the number of sampling points in the azimuth direction N a , the number of sampling points in the range direction N r , the signal sampling rate f s , the signal bandwidth Bw, and the frequency modulation Slope b, pulse repetition frequency PRF, reference slant distance R ref , Doppler center frequency fd 0 , Doppler modulation frequency f r0 , satellite velocity P v , equivalent slant angle , signal wavelength λ, signal carrier frequency f 0 , signal propagation speed c;
步骤二:将二维原始回波复数据Sstart进行方位向解线性调频处理,具体可以分为以下几个步骤:Step 2: Perform azimuth dechirp processing on the two-dimensional original echo data S start , which can be specifically divided into the following steps:
(a)构造两个一维序列i,j,其中i代表方位向序列(行),j代表距离向序列(列);(a) Construct two one-dimensional sequences i,j, where i represents the azimuth sequence (row), and j represents the distance sequence (column);
i=[1,2,…,Na] (2)i=[1,2,...,N a ] (2)
j=[1,2,…,Nr]j=[1,2,…,N r ]
(b)获取二维原始回波复数据Sstart各行对应的方位时刻t(i);(b) Obtain the azimuth time t(i) corresponding to each row of the two-dimensional original echo data S start ;
(c)将二维原始回波复数据Sstart同去旋转因子H1相乘,得到数据S1_1(i,j),其中因子H1(i)是大小为Na×1的一维复数组,公式为:(c) Multiply the two-dimensional original echo complex data S start with the derotation factor H 1 to obtain the data S 1_1 (i,j), where the factor H 1 (i) is a one-dimensional complex number with a size of N a ×1 group, the formula is:
H1(i)=exp{jπ(fr0·t2(i)+2·fd0·t(i))} (4)H 1 (i)=exp{jπ(fr 0 t 2 (i)+2 fd 0 t(i))} (4)
则二维复数组S1_1可由下式得出:Then the two-dimensional complex array S 1_1 can be obtained by the following formula:
S1_1(i,j)=Sstart(i,j)·H1(i) (5)S 1_1 (i, j) = S start (i, j) · H 1 (i) (5)
(d)对复数据S1_1沿每个距离向(按列)进行快速傅里叶变化(FFT),得到复数据S1_2;(d) Perform fast Fourier transform (FFT) on complex data S 1_1 along each distance direction (by column) to obtain complex data S 1_2 ;
S1_2(:,j)=FFT(S1_1(:,j)) (6)S 1_2 (:, j) = FFT(S 1_1 (:, j)) (6)
其中,S1_2(:,j)表示S1_2的第n列,S1_1(:,j)表示S1_1的第n列,FFT(·)表示对一维数组进行快速傅里叶变换。Among them, S 1_2 (:, j) represents the nth column of S 1_2 , S 1_1 (:, j) represents the nth column of S 1_1 , and FFT(·) represents the fast Fourier transform of a one-dimensional array.
(e)获取去旋转后的等效脉冲重复频率PRF';(e) Obtain the equivalent pulse repetition frequency PRF' after derotation;
(g)结合式(7)获取二维复数据每行对应的方位时刻t1(i);(g) Combining formula (7) to obtain the azimuth time t 1 (i) corresponding to each row of the two-dimensional complex data;
(h)将复数据S1_2同因子H2相乘,得到最终方位向解线性调频后的数据S1。其中因子H2(i)是大小为Na×1的一维复数组,其公式为:(h) Multiply the complex data S 1_2 by the factor H 2 to obtain the final azimuth dechirped data S 1 . The factor H 2 (i) is a one-dimensional complex array with a size of N a ×1, and its formula is:
则二维复数组S1可由下式得出:Then the two-dimensional complex array S 1 can be obtained by the following formula:
S1(i,j)=S1_2(i,j)·H2(i) (10)S 1 (i, j) = S 1_2 (i, j) · H 2 (i) (10)
步骤三:将步骤二得到的复数据S1(i,j)沿每个距离向(按列)进行快速傅里叶变换(FFT),得到方位向频谱复数据S2(i,j);Step 3: Perform fast Fourier transform (FFT) on the complex data S 1 (i,j) obtained in Step 2 along each distance direction (column), and obtain the complex data S 2 (i,j) of the azimuth spectrum;
S2(:,j)=FFT(S1(:,j)) (11)S 2 (:,j)=FFT(S 1 (:,j)) (11)
其中,S2(:,j)表示S2的第j列,S1(:,j)表示S1的第j列,FFT(·)表示对一维数组进行快速傅里叶变换。Among them, S 2 (:, j) represents the jth column of S 2 , S 1 (:, j) represents the jth column of S 1 , and FFT(·) represents the fast Fourier transform of a one-dimensional array.
步骤四:将步骤三得到的复数据S2(i,j)同对应方位时刻的方位向解线性调频残留相位误差补偿因子Ω1(i)相乘,得到补偿后的复数据S3(i,j);Step 4: Multiply the complex data S 2 (i,j) obtained in Step 3 with the azimuth dechirp residual phase error compensation factor Ω 1 (i) at the corresponding azimuth moment to obtain the compensated complex data S 3 (i ,j);
(a)结合式(7)获取二维方位向频域距离向时域复数据S2(i,j)每行对应的方位频率fa(i);(a) Combining formula (7) to obtain the azimuth frequency f a (i) corresponding to each row of the two-dimensional azimuth frequency domain distance time domain complex data S 2 (i,j);
(b)结合式(12)获取大小为Na×1的一维补偿因子Ω1(i);(b) Combining formula (12) to obtain a one-dimensional compensation factor Ω 1 (i) whose size is N a ×1;
(c)获取补偿后的二维复数据S3(i,j);(c) Obtain the compensated two-dimensional complex data S 3 (i,j);
S3(i,j)=S2(i,j)·Ω1(i) (14)S 3 (i, j) = S 2 (i, j)·Ω 1 (i) (14)
步骤五:将步骤四得到的复数据S3(i,j)沿每个方位时刻(按行)进行快速傅里叶变换(FFT),得到二维频谱复数据S4(i,j);Step 5: Perform fast Fourier transform (FFT) on the complex data S 3 (i,j) obtained in Step 4 along each azimuth time (by row) to obtain two-dimensional spectrum complex data S 4 (i,j);
S4(i,:)=FFT(S3(i,:)) (15)S 4 (i,:) = FFT(S 3 (i,:)) (15)
其中,S3(i,:)表示S3的第i行,S4(i,:)表示S4的第i行。Wherein, S 3 (i,:) represents the i-th row of S 3 , and S 4 (i,:) represents the i-th row of S 4 .
步骤六:将步骤五得到的复数据S4(i,j)同对应的一致压缩因子Ω2(i,j)相乘,得到粗聚焦复数据S5(i,j)。Step 6: Multiply the complex data S 4 (i,j) obtained in Step 5 by the corresponding consistent compression factor Ω 2 (i,j) to obtain coarse-focus complex data S 5 (i,j).
(a)根据参考斜距Rref获取最短斜距Rmin;(a) Obtain the shortest slant distance R min according to the reference slant distance R ref ;
(b)获取二维频域复数据S4(i,j)每列对应的距离频域fτ(j);(b) Obtain the distance frequency domain f τ (j) corresponding to each column of the two-dimensional frequency domain complex data S 4 (i,j);
(c)结合式(12)与式(17)获取二维频域复数据S4(i,j)每列对应的方位向波数kx(i)与每行对应的距离向波数krc(j);(c) Combining Equation (12) and Equation (17) to obtain the two-dimensional frequency domain complex data S 4 (i,j), the azimuth wavenumber k x (i) corresponding to each column and the range wavenumber k rc ( j);
(d)结合式(16)~式(18)获取大小为Na×Nr的二维一致压缩因子Ω2(i,j);(d) Combining formulas (16) to (18) to obtain a two-dimensional consistent compression factor Ω 2 (i,j) with a size of N a ×N r ;
(e)结合式(19)获取一致压缩后的二维复数据S5(i,j);(e) Obtain consistent compressed two-dimensional complex data S 5 (i,j) by combining formula (19);
S5(i,j)=S4(i,j)·Ω2(i,j) (20)S 5 (i, j) = S 4 (i, j)·Ω 2 (i, j) (20)
步骤七:对于步骤六得到的复数据S5(i,j),利用sinc插值法进行stolt插值处理,得到由二维频域映射到二维波数域的复数据S6(i,j);Step 7: For the complex data S 5 (i, j) obtained in Step 6, use the sinc interpolation method to perform stolt interpolation processing, and obtain the complex data S 6 (i, j) mapped from the two-dimensional frequency domain to the two-dimensional wavenumber domain;
(a)根据距离频域到距离波数域的映射关系,结合式(18)获取距离波数域波数k'rc(i,j);(a) According to the mapping relationship from the distance frequency domain to the distance wavenumber domain, combined with formula (18) to obtain the wavenumber k' rc (i,j) in the distance wavenumber domain;
(b)遍历获取距离波数域波数k'rc(i,j)的最大值k'rc,max与最小值k'rc,max,并获取距离波数域波数等分间隔Δk'rc;(b) Traverse to obtain the maximum value k' rc ,max and the minimum value k' rc,max of the wavenumber k' rc (i,j) in the distance wavenumber domain, and obtain the equal interval Δk' rc of the wavenumber in the distance wavenumber domain;
(c)获取二维波数域数据均匀的距离波数域波数 (c) Obtain the uniform distance wavenumber domain wavenumber of the two-dimensional wavenumber domain data
(d)获取二维波数域复数据各均匀的距离波数域波数在每行对应的不均匀k'rc(i,:)中的位置p(i,j)。(d) Obtain the uniform distance wavenumber domain wavenumber of the two-dimensional wavenumber domain complex data Position p(i,j) in uneven k' rc (i,:) corresponding to each row.
方法为按行进行下列操作:以获取第一行第一列的位置p(1,1)为例,首先获取绝对差值n=[1,2,…,Nr],获取最小的绝对差值Δkmin和对应位置的n,若
以此类推,得到每一个位置p(i,j)。By analogy, each position p(i,j) is obtained.
(e)结合上步得到的位置p(i,j),获取sinc插值所需采样点间隔q(i,j,n);(e) Combining the position p(i,j) obtained in the previous step, obtain the sampling point interval q(i,j,n) required for sinc interpolation;
(f)结合式(24)利用sinc插值法,获取出经stolt插值后的二维数据S6,由于二维数据是复数据,需要分别对S6(i,j)的实部S6_re(i,j)和虚部S6_im(i,j)分别进行sinc插值法获取得出。 ( f) Combining formula (24) with the sinc interpolation method to obtain the two-dimensional data S 6 after stolt interpolation, since the two-dimensional data is complex data, the real part S 6_re ( i, j) and the imaginary part S 6_im (i, j) are obtained by sinc interpolation method respectively.
其中,N是插值核长度,sinc(·)是指插值函数S5_re(i,j)是指二维数据S5_re第i行第j列的实部,S5_im(i,j)是指二维数据S5_im第i行第j列的虚部。Among them, N is the interpolation kernel length, sinc( ) refers to the interpolation function S 5_re (i,j) refers to the real part of the i-th row and j-th column of the two-dimensional data S 5_re , and S 5_im (i,j) refers to the imaginary part of the i-th row and j-th column of the two-dimensional data S 5_im .
步骤八:将步骤七得到的复数据S6(i,j)沿每个距离向(按列)进行快速傅里叶逆变换(IFFT),得到方位时域距离波数域复数据S7(i,j);Step 8: Perform Inverse Fast Fourier Transform (IFFT) on the complex data S 6 (i,j) obtained in Step 7 along each distance direction (column), and obtain complex data S 7 (i ,j);
S7(:,j)=IFFT(S6(:,j)) (27)S 7 (:, j) = IFFT (S 6 (:, j)) (27)
其中,S6(:,j)表示S6的第j列,S7(:,j)表示S7的第j列,IFFT(·)表示对一维数组进行快速傅里叶逆变换。Among them, S 6 (:, j) represents the j-th column of S 6 , S 7 (:, j) represents the j-th column of S 7 , and IFFT (·) represents the inverse fast Fourier transform of a one-dimensional array.
步骤九:将步骤八得到的复数据S7(i,j)同几何校正因子Ω3(i,j)相乘,得到经几何校正后的复数据S8(i,j);Step 9: Multiply the complex data S 7 (i,j) obtained in Step 8 by the geometric correction factor Ω 3 (i,j) to obtain complex data S 8 (i,j) after geometric correction;
(a)结合式(8)与式(12),获取几何校正因子Ω4(i,j);(a) Combine formula (8) and formula (12) to obtain geometric correction factor Ω 4 (i,j);
(b)利用式(30)获取经几何校正后的复数据S8(i,j);(b) Use formula (30) to obtain geometrically corrected complex data S 8 (i,j);
S8(i,j)=S7(i,j)·Ω3(i,j) (29)S 8 (i, j) = S 7 (i, j)·Ω 3 (i, j) (29)
步骤十:将步骤九得到的复数据S8(i,j)沿每个方位时刻(按行)进行快速傅里叶逆变换(IFFT),得到最终的成像结果Send(i,j);Step 10: Perform Inverse Fast Fourier Transform (IFFT) on the complex data S 8 (i,j) obtained in Step 9 along each azimuth moment (by row) to obtain the final imaging result S end (i,j);
Send(i,:)=IFFT(S8(i,:)) (30)S end (i,:)=IFFT(S 8 (i,:)) (30)
其中,S8(i,:)表示S8的第i行,Send(i,:)表示Send的第i行。Wherein, S 8 (i,:) represents the i-th row of S 8 , and S end (i,:) represents the i-th row of S end .
实施例:Example:
本实施例提出一种基于滑动接收窗的机载高分辨率斜视聚束SAR成像方法,仿真场景为3×3点阵,其点与点的间隔为100m,最终分别对仿真场景中左上、中间、右下三个点进行了评估,具体仿真场景如图2所示,其成像过程中涉及的成像参数如表1所示。This embodiment proposes an airborne high-resolution squint spotlight SAR imaging method based on a sliding receiving window. The simulation scene is a 3×3 dot matrix, and the interval between points is 100m. Finally, the upper left and middle of the simulation scene are respectively , and the lower right three points were evaluated. The specific simulation scene is shown in Figure 2, and the imaging parameters involved in the imaging process are shown in Table 1.
表1实施例参数Table 1 embodiment parameters
本实施例具体包括以下步骤:This embodiment specifically includes the following steps:
步骤一:读入基于滑动接收窗的机载高分辨率斜视聚束SAR二维原始回波复数据Sstart以及相应的成像参数。其中,Sstart是二维复数组,大小为65536×16384,具体成像参数如表1所示;Step 1: Read in the airborne high-resolution squint spotlight SAR two-dimensional original echo complex data S start and the corresponding imaging parameters based on the sliding receiving window. Among them, S start is a two-dimensional complex array with a size of 65536×16384, and the specific imaging parameters are shown in Table 1;
步骤二:将二维原始回波复数据Sstart进行方位向解线性调频处理,具体操作步骤为:Step 2: Perform azimuth dechirp processing on the two-dimensional original echo data S start . The specific operation steps are:
(a)构造一维序列,如式(2)所示,i=[1,2,…,65536],j=[1,2,…,16384];(a) Construct a one-dimensional sequence, as shown in formula (2), i=[1,2,…,65536], j=[1,2,…,16384];
(b)获取二维原始回波复数据Sstart每行对应的方位时刻t(i),具体过程按式(3)进行;(b) Obtain the azimuth time t(i) corresponding to each line of the two-dimensional original echo data S start , and the specific process is carried out according to formula (3);
(c)将数据Sstart同去旋转因子H1(i)相乘,得到数据S1_1(i,j)。其中因子H1是大小为65536×1的一维复数组,具体获取过程按式(4)进行,而二维复数组S1_1(i,j)获取过程按式(5)进行;(c) Multiply the data S start by the derotation factor H 1 (i) to obtain the data S 1_1 (i,j). The factor H 1 is a one-dimensional complex array with a size of 65536×1. The specific acquisition process is carried out according to formula (4), while the two-dimensional complex array S 1_1 (i,j) is obtained according to formula (5);
(d)对复数据S1_1(i,j)按式(6)沿每个距离向进行快速傅里叶变化(FFT),得到复数据S1_2(i,j);(d) Perform fast Fourier transformation (FFT) on the complex data S 1_1 (i,j) according to formula (6) along each distance direction to obtain the complex data S 1_2 (i,j);
(e)获取去旋转后的等效脉冲重复频率PRF',获取过程按式(7)进行;(e) Obtain the equivalent pulse repetition frequency PRF' after derotation, and the acquisition process is carried out according to formula (7);
(g)结合式(7)获取二维复数据每行对应的方位时刻t1(i),获取过程按式(8)进行;(g) Combining formula (7) to obtain the azimuth time t 1 (i) corresponding to each row of two-dimensional complex data, the acquisition process is carried out according to formula (8);
(h)将数据S1_2(i,j)同因子H2(i)相乘,得到最终方位向解线性调频后的数据S1(i,j)。其中因子H2(i)是大小为65536×1的一维复数组,其获取过程按式(9)进行,而二维复数组S1获取过程按式(10)进行;(h) Multiply the data S 1_2 (i,j) with the factor H 2 (i) to obtain the final azimuth dechirped data S 1 (i,j). Among them, the factor H 2 (i) is a one-dimensional complex array with a size of 65536×1, and its acquisition process is carried out according to formula (9), while the acquisition process of the two-dimensional complex array S 1 is carried out according to formula (10);
步骤三:将步骤二得到的复数据S1(i,j)沿每个距离向(按列)进行快速傅里叶变换(FFT),得到方位向频谱复数据S2(i,j),具体操作过程按式(11)进行;Step 3: Perform fast Fourier transform (FFT) on the complex data S 1 (i,j) obtained in Step 2 along each distance direction (column), and obtain the complex data S 2 (i,j) in the azimuth direction. The specific operation process is carried out according to formula (11);
步骤四:将步骤三得到的复数据S2(i,j)同对应方位时刻的方位向解线性调频残留相位误差补偿因子Ω1(i)相乘,得到补偿后的复数据S3(i,j);Step 4: Multiply the complex data S 2 (i,j) obtained in Step 3 with the azimuth dechirp residual phase error compensation factor Ω 1 (i) at the corresponding azimuth moment to obtain the compensated complex data S 3 (i ,j);
(a)获取二维方位向频域距离向时域复数据S2(i,j)每行对应的方位频率fa,具体获取过程按式(12)进行;(a) Obtain the azimuth frequency f a corresponding to each row of the two-dimensional azimuth, frequency domain, distance and time domain complex data S 2 (i,j), and the specific acquisition process is carried out according to formula (12);
(b)结合式(7)获取大小为65536×1的一维补偿因子Ω1(i),具体获取过程按式(13)进行;(b) Combining formula (7) to obtain a one-dimensional compensation factor Ω 1 (i) with a size of 65536×1, the specific acquisition process is carried out according to formula (13);
(c)获取补偿后的二维复数据S3(i,j),具体获取过程按式(14)进行;(c) Obtain the compensated two-dimensional complex data S 3 (i,j), the specific acquisition process is carried out according to formula (14);
步骤五:将步骤四得到的复数据S3(i,j)沿每个方位时刻(按行)进行快速傅里叶变换(FFT),得到二维频谱复数据S4(i,j),具体操作过程按式(15)进行;Step 5: Perform fast Fourier transform (FFT) on the complex data S 3 (i,j) obtained in Step 4 along each azimuth moment (by row) to obtain the two-dimensional spectrum complex data S 4 (i,j), The specific operation process is carried out according to formula (15);
步骤六:将步骤五得到的复数据S4(i,j)同对应的一致压缩因子Ω2(i,j)相乘,得到粗聚焦复数据S5(i,j)。Step 6: Multiply the complex data S 4 (i,j) obtained in Step 5 by the corresponding consistent compression factor Ω 2 (i,j) to obtain coarse-focus complex data S 5 (i,j).
(a)根据参考斜距Rref=19.31km获取最短斜距Rmin,具体获取过程按式(16)进行;(a) Obtain the shortest slant distance R min according to the reference slant distance R ref =19.31km, and the specific acquisition process is carried out according to formula (16);
(b)获取二维频域复数据S4(i,j)每列对应的距离频域fτ(j),具体获取过程按式(17)进行;(b) Obtain the distance frequency domain f τ (j) corresponding to each column of the two-dimensional frequency domain complex data S 4 (i,j), and the specific acquisition process is carried out according to formula (17);
(c)结合式(7)与式(11)获取二维频域复数据S4(i,j)每列对应的方位向波数kx(i)与每行对应的距离向波数krc(j),具体获取过程按式(18)进行;(c) Combining formula (7) and formula (11) to obtain the two-dimensional frequency domain complex data S 4 (i,j) corresponding to the azimuth wave number k x (i) of each column and the range wave number k rc ( j), the specific acquisition process is carried out according to formula (18);
(d)结合式(10)~式(12)获取大小为65536×16384的二维一致压缩因子Ω2(i,j),具体获取过程按式(19)进行;(d) Obtain the two-dimensional uniform compression factor Ω 2 (i, j) with a size of 65536×16384 by combining formulas (10) to (12), and the specific acquisition process is carried out according to formula (19);
(e)结合式(13)获取一致压缩后的二维复数据S5(i,j),具体获取过程按式(20)进行;(e) Obtain consistent compressed two-dimensional complex data S 5 (i,j) in combination with formula (13), and the specific acquisition process is carried out according to formula (20);
步骤七:对于步骤六得到的复数据S5(i,j),利用sinc插值法进行stolt插值处理,得到由二维频域映射到二维波数域的复数据S6(i,j);Step 7: For the complex data S 5 (i, j) obtained in Step 6, use the sinc interpolation method to perform stolt interpolation processing, and obtain the complex data S 6 (i, j) mapped from the two-dimensional frequency domain to the two-dimensional wavenumber domain;
(a)根据距离频域到距离波数域的映射关系,结合式(18)获取距离波数域波数k'rc(i,j),具体获取过程按式(21)进行;(a) According to the mapping relationship from the distance frequency domain to the distance wavenumber domain, the wavenumber k' rc (i, j) in the distance wavenumber domain is obtained by combining formula (18), and the specific acquisition process is carried out according to formula (21);
(b)遍历获取距离波数域波数k'rc(i,j)的最大值k'rc,max=69.12rad/s与最小值k'rc,max=-105.06rad/s,并获取距离波数域波数等分间隔Δk'rc,具体操作按式(22)进行;(b) Traverse to obtain the maximum value k' rc,max =69.12rad/s and the minimum value k' rc,max =-105.06rad/s of the wavenumber k' rc (i,j) in the distance wavenumber domain, and obtain the distance wavenumber domain The wave number equal interval Δk' rc , the specific operation is carried out according to formula (22);
(c)获取二维波数域复数据均匀的距离波数域波数具体操作按式(23)进行;(c) Obtain the uniform distance wavenumber domain wavenumber of complex data in the two-dimensional wavenumber domain The specific operation is carried out according to formula (23);
(d)获取二维波数域复数据各均匀的距离波数域波数在每行对应的不均匀k'rc(i,:)中的位置p(i,j)。方法为按行进行下列操作:先获取第一行第一列的位置p(1,1),获取绝对差值n=[1,2,…,16384],获取最小的绝对差值Δkmin和对应位置的n,若
以此类推,得到每一个位置p(i,j)。By analogy, each position p(i,j) is obtained.
(e)结合上步得到的位置p(i,j),获取sinc插值所需采样点间隔q(i,j,n),具体操作按式(24)进行;(e) Combining the position p(i,j) obtained in the previous step, obtain the sampling point interval q(i,j,n) required for sinc interpolation, and the specific operation is carried out according to formula (24);
(f)结合式(18)利用sinc插值法,选择sinc插值核长度为N=8,获取出经stolt插值后的二维复数据S6(i,j),由于二维数据是复数数据,需要分别对S6(i,j)的实部S6_re(i,j)和虚部S6_im(i,j)分别进行sinc插值法获取得出,具体操作按式(25)(26)进行。(f) Combining formula (18) with the sinc interpolation method, select the sinc interpolation kernel length as N=8, and obtain the two-dimensional complex data S 6 (i,j) after stolt interpolation. Since the two-dimensional data is complex data, The real part S 6_re (i,j) and the imaginary part S 6_im (i,j) of S 6 (i,j) need to be obtained by sinc interpolation respectively, and the specific operation is carried out according to formula (25) (26) .
步骤八:将步骤七得到的复数据S6(i,j)沿每个距离向(按列)进行快速傅里叶逆变换(IFFT),得到方位时域距离波数域复数据S7(i,j),具体操作按式(27)进行;Step 8: Perform Inverse Fast Fourier Transform (IFFT) on the complex data S 6 (i,j) obtained in Step 7 along each distance direction (column), and obtain complex data S 7 (i ,j), the specific operation is carried out according to formula (27);
步骤九:将步骤八得到的复数据S7(i,j)同几何校正因子Ω3(i,j)相乘,得到经几何校正后的复数据S8(i,j);Step 9: Multiply the complex data S 7 (i,j) obtained in Step 8 by the geometric correction factor Ω 3 (i,j) to obtain complex data S 8 (i,j) after geometric correction;
(a)结合式(8)与式(12),获取几何校正因子Ω3(i,j),具体操作按式(28)进行;(a) Combine formula (8) and formula (12) to obtain the geometric correction factor Ω 3 (i,j), and the specific operation is carried out according to formula (28);
(b)利用式(28)获取经几何校正后的复数据S8(i,j),具体操作按式(29)进行;(b) Use formula (28) to obtain geometrically corrected complex data S 8 (i, j), and the specific operation is carried out according to formula (29);
步骤十:将步骤九得到的复数据S8(i,j)沿每个方位时刻(按行)进行快速傅里叶逆变换(IFFT),得到最终的成像结果Send(i,j),具体操作按式(30)进行;Step 10: Perform Inverse Fast Fourier Transform (IFFT) on the complex data S 8 (i,j) obtained in Step 9 along each azimuth moment (by row) to obtain the final imaging result S end (i,j), The specific operation is carried out according to formula (30);
经过上述步骤的成像处理,得到最终的场景成像结果如图3所示。表2给出了场景左上、中间、右下三个点目标的成像评估结果,图4、图5、图6分别给出了场景左上、中间、右下三个点目标的剖面图。After the imaging processing of the above steps, the final scene imaging result is obtained as shown in FIG. 3 . Table 2 shows the imaging evaluation results of the three point targets in the upper left, middle, and lower right of the scene. Figure 4, Figure 5, and Figure 6 respectively show the cross-sectional views of the three point targets in the upper left, middle, and lower right of the scene.
表二成像评估结果Table 2 Imaging evaluation results
根据表2评估结果以及图4~图6所示剖面图,可以得出:一方面,该成像方法在斜视角度为70度时仍然能够精确聚焦,说明本发明提出的方法不受斜视角度的限制;另一方面,该成像方法对于0.1m超高分辨仍然能够精确聚焦,说明本发明提出的方法能够对目前各种分辨率实现精确聚焦。因此,本发明所提出的方法可以实现基于滑动接收窗的机载高分辨率斜视角聚束SAR精确成像,得到了高精度的成像结果。According to the evaluation results in Table 2 and the cross-sectional diagrams shown in Figures 4 to 6, it can be concluded that: on the one hand, the imaging method can still focus accurately when the squint angle is 70 degrees, which shows that the method proposed by the present invention is not limited by the squint angle On the other hand, the imaging method can still accurately focus for 0.1m ultra-high resolution, indicating that the method proposed by the present invention can achieve accurate focus for various resolutions at present. Therefore, the method proposed in the present invention can realize accurate imaging of airborne high-resolution oblique-angle spotlight SAR based on a sliding receiving window, and obtain high-precision imaging results.
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