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高分辨稀疏表示及其在雷达动目标检测中的应用

陈小龙 关键 何友 于晓涵

陈慧, 田湘, 李子豪, 等. 共形FDA-MIMO雷达降维目标参数估计研究[J]. 雷达学报, 2021, 10(6): 811–821. DOI: 10.12000/JR21197
引用本文: 陈小龙, 关键, 何友, 于晓涵. 高分辨稀疏表示及其在雷达动目标检测中的应用[J]. 雷达学报, 2017, 6(3): 239-251. doi: 10.12000/JR16110
CHEN Hui, TIAN Xiang, LI Zihao, et al. Reduced-dimension target parameter estimation for conformal FDA-MIMO radar[J]. Journal of Radars, 2021, 10(6): 811–821. DOI: 10.12000/JR21197
Citation: Chen Xiaolong, Guan Jian, He You, Yu Xiaohan. High-resolution Sparse Representation and Its Applications in Radar Moving Target Detection[J]. Journal of Radars, 2017, 6(3): 239-251. doi: 10.12000/JR16110

高分辨稀疏表示及其在雷达动目标检测中的应用

DOI: 10.12000/JR16110
基金项目: 国家自然科学基金(61501487, 61401495, U1633122, 61471382, 61531020),山东省自然科学基金(2015ZRA06052),航空基金(20162084005, 20162084006, 20150184003),中国科协“青年人才托举工程”和“泰山学者”专项经费
详细信息
    作者简介:

    陈小龙(1985–),男,山东烟台人,博士,海军航空工程学院电子信息工程系讲师。承担国家自然科学基金等项目7项,发表学术论文50余篇,授权国家发明专利13项。获中国电子学会优秀博士学位论文奖、入选中国科协“青年人才托举工程” 。研究方向为雷达动目标检测、海杂波抑制、雷达信号精细化处理等。E-mail: cxlcxl1209@163.com

    关 键(1968–),男,辽宁锦州人,教授,博士生导师,海军航空工程学院电子信息工程系主任。承担973、国家自然科学基金、国防预研等项目20余项。发表论文140余篇,出版学术专著2部,获国家发明专利22项。获全国优秀博士学位论文奖,获得国家科技进步二等奖1项、军队科技进步一等奖2项,山东省技术发明一等奖1项; “百千万人才工程” 国家级人选,入选教育部新世纪优秀人才支持计划,“泰山学者” 特聘教授。主要研究方向为雷达目标检测与跟踪、侦察图像处理和信息融合。E-mail: guanjian96@tsinghua.org.com

    何 友(1956–),男,吉林磐石人,中国工程院院士,教授,博士生导师,海军航空工程学院信息融合研究所所长。主要研究领域有雷达目标检测方法、多传感器信息融合、多目标跟踪、分布检测理论及应用、军事大数据等

    于晓涵(1991–),女,河北沧州人,博士生,海军航空工程学院信息融合研究所。研究方向为雷达动目标检测、海杂波抑制、雷达视频跟踪等。E-mail: 2953164562@qq.com 

    通讯作者:

    陈小龙   cxlcxl1209@163.com

    关键   guanjian96@tsinghua.org.com

  • 中图分类号: TN957.51

High-resolution Sparse Representation and Its Applications in Radar Moving Target Detection

Funds: The National Natural Science Foundation of China (61501487, 61401495, U1633122, 61471382, 61531020), The Natural Science Foundation of Shandong Province (2015ZRA06052), The Aeronautical Science Foundation of China (20162084005, 20162084006, 20150184003), The Young Elite Scientist Program of CAST and Special Funds of Taishan Scholars
  • 摘要: 复杂背景下稳健高效的低可观测动目标检测始终是雷达信号处理领域的研究热点和难点,一方面,强杂波背景和目标复杂运动使得信号微弱,时频域难以区分;另一方面,相参积累算法复杂,长时间积累运算量较大,如何利用有限的雷达资源提高雷达探测性能成为亟需解决的问题。高分辨稀疏表示技术从信号稀疏性角度出发区分杂波和动目标,是传统变换域动目标检测技术的拓展,具有高时频分辨率、对噪声不敏感、稳健性高以及适于多分量信号分析的优势,有广阔应用前景。该文重点从应用角度进行归纳总结,系统回顾了雷达动目标检测的常规方法,然后对稀疏表示在雷达杂波特性分析、抑制、动目标检测、特征提取、时频分析等方面的应用进行了初步总结和归纳,对研究方向进行展望,最后结合实测数据和已有成果给出了部分处理结果。

     

  • In recent years, Frequency Diverse Array (FDA) radar has received much attention due to its range-angle-time-dependent beampattern[1,2]. Combining the advantages of FDA and traditional phased array Multiple-Input Multiple-Output (MIMO) radar in the degree of freedom, the FDA Multiple-Input Multiple Output (FDA-MIMO) radar was proposed in Ref. [3] and applied in many fields[4-9]. For parameter estimation algorithm, the authors first proposed a FDA-MIMO target localization algorithm based on sparse reconstruction theory[10], and an unbiased joint range and angle estimation method was proposed in Ref. [11]. The work of Ref. [12] further proved that the FDA-MIMO is superior to traditional MIMO radar in range and angle estimation performance, and the authors of Ref. [13] introduced a super-resolution MUSIC algorithm for target location, and analyzed its resolution threshold. Meanwhile, high-resolution Doppler processing is utilized for moving target parameter estimation[14]. The Estimation of Signal Parameters via Rotational Invariance Technique (ESPRIT) and PARAllel FACtor (PARAFAC) was proposed in Ref. [15], which is a search-free algorithm for FDA-MIMO.

    Moreover, the research of conformal array has received more and more attention. Conformal array is a non-planar array that can be completely attached to the surface of the carrier[16]. It has significant advantages such as reducing the aerodynamic impact on the carrier and smaller radar cross section[17]. In addition, conformal array can achieve wide-angle scanning with a lower SideLobe Level (SLL)[18]. Different from traditional arrays, the element beampattern of conformal array needs to be modeled separately in the parameter estimation due to the difference of carrier curvature[19-21].

    As far as we know, most of the existing researches on FDA-MIMO are based on linear array, while there is little research on the combination of FDA-MIMO and conformal array[22]. In this paper, we replace the receiving array in the traditional FDA-MIMO with conformal array. Compared with conventional FDA-MIMO, conformal FDA-MIMO inherits the merits of conformal array and FDA-MIMO, which can effectively improve the stealth and anti-stealth performance of the carrier, and reduce the volume and the air resistance of the carrier. For conformal FDA-MIMO, we further study the parameters estimation algorithm. The major contributions of this paper are summarized as follows:

    (1) A conformal FDA-MIMO radar model is first formulated.

    (2) The parameter estimation Cramér-Rao Lower Bound (CRLB) for conformal FDA-MIMO radar is derived.

    (3) Inspired by the existing work of Refs. [23,24], a Reduced-Dimension MUSIC (RD-MUSIC) algorithm for conformal FDA-MIMO radar is correspondingly proposed to reduce the complexity.

    The rest of the paper consists of four parts. Section 2 formulates the conformal FDA-MIMO radar model, and Section 3 derives a RD-MUSIC algorithm for conformal FDA-MIMO radar. Simulation results for conformal FDA-MIMO radar with semi conical conformal receiving array are provided in Section 4. Finally, conclusions are drawn in Section 5.

    For the convenience of analysis, we consider a monostatic conformal FDA-MIMO radar which is composed by a M-element linear FDA transmitting array and a N-element conformal receiving array, as shown in Fig. 1. d denotes the inter-element spacing, the carrier frequency at the mth transmitting element is fm=f1+Δf(m1), m=1,2,,M where f1 is the transmission frequency of the first antenna element, which is called as reference frequency, and Δf is the frequency offset between the adjacent array elements.

    Figure  1.  Conformal FDA-MIMO radar

    The complex envelope of the transmitted signal of the mth transmitting element is denoted as φm(t), assume the transmitting waveforms have orthogonality,

    Tpφm(t)φm1(tτ)dt=0,m1m (1)

    where τ denotes the time delay, Tp denotes the pulse duration, and () is conjugate operator. The signal transmitted from the mth element can be expressed as

    sm(t)=am(t,θ,ϕ,r)φm(t),0tTp (2)

    where

    am(t,θ,ϕ,r)=exp{j2π((m1)Δfrcf1(m1)dsinαc(m1)Δft)} (3)

    is the mth element of the transmitting steering vector according to the phase difference between adjacent elements, the angle between far-field target and transmitting array is denoted as α=arcsin(sinθcosϕ), where arcsin() denotes arcsine operator, α can be calculated by using the inner product between the target vector and unit vector along the X-axis. θ,ϕ,r are the elevation, azimuth and range between the target and the origin point, respectively. The phase difference between adjacent elements is

    Δψt0=2π(Δfrcf1dsinαcΔft) (4)

    where c is light speed. For far-field target P(r,θ,ϕ), the transmitting steering vector is

    a0(t,θ,ϕ,r)=[1,exp{jΔψt0},,exp{j(M1)Δψt0}]T (5)

    For the conformal receiving array, as shown in Fig. 1(b), the time delay between target P(r,θ,ϕ) and the nth receiving array element is

    τn=rn/c (6)

    where rn is the range between target and the nth receiving array element. For far-field assumption, the rn can be approximated as

    rnrpnr (7)

    where r denotes the range between the target and the origin point, pn=xnex+yney+znez denotes the position vector from the nth element to origin point, and r=sinθcosϕex+sinθsinϕey+cosθez is the unit vector in target orientation, where ex,ey and ez are the unit vectors along the X- , Y- , and Z-axis, respectively. (xn,yn,zn) are the coordinates of the nth element in the Cartesian coordinate system. For simplicity, we let u=sinθcosϕ, v=sinθcosϕ, so the time delay τn=(r(uxn+vyn+cosθzn))/c. The time delay between the first element and the nth element at the receiving array is expressed as

    Δτrn=τ1τn=u(xnx1)+v(yny1)+cosθ(znz1)c (8)

    And the corresponding phase difference between the first element and the nth element is

    ΔψRn=2πf1Δτrn (9)

    Consequently, the receiving steering vector is

    b(θ,ϕ)=[r1(θ,ϕ),r2(θ,ϕ)exp(jΔψr2),,rN(θ,ϕ)exp(jΔψrN)]T (10)

    where rn(θ,ϕ) is the nth conformal receiving array element beampattern which should be designed in its own local Cartesian coordinate system. In this paper, we utilize Euler rotation method to establish transformation frame between local coordinate system and global coordinate system[25,26].

    Then the total phase difference between adjacent transmitting array elements can be rewritten as

    Δψt=2π(Δf2rcf1dsinαcΔft) (11)

    where the factor 2r in the first term represents the two-way transmission and reception, and the correspondingly transmitting steering vector is written as

    a(t,θ,ϕ,r)=[1,exp{jΔψt},,exp{j(M1)Δψt}]T (12)

    Assuming L far-field targets are located at (θi,ϕi,Ri), i=1,2,,L and snapshot number is K. After matched filtering, the received signal can be formulated as following matrix (13,14)

    X=AS+N (13)

    where the array manifold A is expressed as

    A=[at,r(θ1,ϕ1,r1),,at,r(θL,ϕL,rL)]=[b(θ1,ϕ1)a(θ1,ϕ1,r1),,b(θL,ϕL)a(θL,ϕL,rL)] (14)

    where at,r(θ,ϕ,r) is the joint transmitting-receiving steering vector, S=[s(t1),s(t2),,s(tK)]CL×K and NCMN×K denote the signal matrix and noise matrix, respectively, where noise follows the independent identical distribution, and denotes Kronecker product.

    a(θ,ϕ,r)=[1exp{j2π(2Δfrcf1dsinαc)}exp{j2π(M1)(2Δfrcf1dsinαc)}] (15)

    which can be expressed as

    a(θ,ϕ,r)=a(θ,ϕ)a(r) (16)

    where

    a(r)=[1,exp(j2π2Δfrc),,exp(j2π(M1)2Δfrc)]T (17)
    a(θ,ϕ)=[1,exp(j2πf1dsinαc),,exp[j2π(M1)f1dsinαc]]T (18)

    and represents Hadamard product operator.

    The CRLB can be obtained from the inverse of Fisher information matrix[27,28], which establishes a lower bound for the variance of any unbiased estimator. We employ the CRLB for conformal FDA-MIMO parameter estimation to evaluate the performance of some parameter estimation algorithms.

    The discrete signal model is

    x[k]=at,r(θ,ϕ,r)s[k]+N[k],k=1,2,,K (19)

    For the sake of simplification, we take at,r as the abbreviation of at,r(θ,ϕ,r).

    The Probability Distribution Function (PDF) of the signal model with K snapshots is

    p(x|θ,ϕ,r)=1(2πσ2n)K2exp(1σ2n(xat,rs)H(xat,rs)) (20)

    where x=[x(1),x(2),,x(K)] and s=[s(1),s(2),,s(K)].

    The CRLB matrix form of elevation angle, azimuth angle and range is given by Eq. (21), diagonal elements {Cθθ,Cϕϕ,Crr} represent CRLB of estimating elevation angle, azimuth angle and range, respectively.

    CRLB=[CθθCθϕCθrCϕθCϕϕCϕrCrθCrϕCrr]=FIM1=[F11F12F13F21F22F23F31F32F33] (21)

    The elements of Fisher matrix can be expressed as

    Fij=E[2ln(p(xθ,ϕ,r))xixj],i,j=1,2,3 (22)

    In the case of K snapshots, PDF can be rewritten as

    p(x|θ,ϕ,r)=Cexp{1σ2nKn=1(x[k]at,rs[k])H(x[k]at,rs[k])} (23)

    where C is a constant, natural logarithm of Eq. (23) is

    ln(p(x|θ,ϕ,r))=ln(C)1σ2nKk=1(x[k]at,rs[k])H(x[k]at,rs[k]) (24)

    where ln() represents the logarithm operator. The first entry of Fisher matrix can be expressed as

    F11=E[2ln(p(x|θ,ϕ,r))θ2] (25)

    Correspondingly, the first derivative of natural logarithm is given by

    ln(p(x|θ,ϕ,r))θ=1σ2nKk=1(xH[k]at,rθs[k]aHt,rθs[k]x[k]+aHt,rθat,rs2[n]a+aHt,rat,rθs2[n]) (26)

    Then we can obtain the second derivative of

    2ln(p(x|θ,ϕ,r))θ2=1σ2nKk=1(x[k]H2at,rθ2s[k]2aHt,rθ2s(k)x[k]+2aHt,rθ2at,rs[k]2+aHt,rθat,rθs[k]2+aHt,rθat,rθs[k]2+aHt,r2at,rθ2s[k]2) (27)

    And then we have

    Kk=1x[k]=Kk=1at,rs[k]+N[k]=at,r(θ,ϕ,r)Kk=1s[k] (28)

    and

    Kk=1s2[k]=Kvar(s[k])=Kσ2s (29)

    where var() is a symbol of variance. Therefore, the PDF after quadratic derivation can be written as

    E[2ln(p(x|θ,ϕ,r))θ2]=Kσ2sσ2n(aHt,rθat,rθ+aHt,rθat,rθ)=2Kσ2sσ2nat,rθ2 (30)

    where denotes 2-norm. Similarly, the other elements of the Fisher matrix can also be derived in the similar way, so the Fisher matrix can be expressed as

    CRLB1=FIM=2Kσ2sσ2n[aθ2FIM12FIM13FIM21aϕ2FIM23FIM31FIM32ar2] (31)

    where

    FIM12=12[aHt,rθat,rϕ+aHt,rϕat,rθ],
    FIM13=12[aHt,rθat,rr+aHt,rrat,rθ],
    FIM21=12[aHt,rϕat,rθ+aHt,rθat,rϕ],
    FIM23=12[aHt,rϕat,rr+aHt,rrat,rϕ],
    FIM31=12[aHt,rrat,rθ+aHt,rθat,rr],
    FIM32=12[aHt,rrat,rϕ+aHt,rϕat,rr],
    σ2sσ2n=SNR

    Finally, the CRLB of conformal FDA-MIMO can be calculated by the inverse of Fisher matrix.

    The covariance matrix of the conformal FDA-MIMO receiving signal can be written as

    RX=ARsAH+σ2IMN (32)

    where Rs represents the covariance matrix of transmitting signal, IMN denotes MN dimensional identity matrix. For independent target signal and noise, RX can be decomposed as

    RX=USΛSUHS+UnΛnUHn (33)

    The traditional MUSIC algorithm is utilized to estimate the three-dimensional parameters {θ,ϕ,r}, MUSIC spectrum can be expressed as

    PMUSIC(θ,ϕ,r)=1aHt,r(θ,ϕ,r)UnUHnat,r(θ,ϕ,r) (34)

    The target location can be obtained by mapping the peak indexes of MUSIC spectrum.

    Traditional MUSIC parameter estimation algorithm is realized by 3D parameter search, which has good performance at the cost of high computational complexity. When the angular scan interval is less than 0.1°, the running time of single Monte-Carlo simulation is in hours, which is unpracticable for us to analysis conformal FDA-MIMO estimation performance by hundreds of simulations.

    In order to reduce the computation complexity of the parameter estimation algorithm for conformal FDA-MIMO, we propose a RD-MUSIC algorithm, which has a significant increase in computing speed at the cost of little estimation performance loss.

    At first, we define

    V(θ,ϕ,r)=aHt,r(θ,ϕ,r)HUnUHnat,r(θ,ϕ,r)=[b(θ,ϕ)a(θ,ϕ,r)]HUnUHn[b(θ,ϕ)a(θ,ϕ,r)] (35)

    Eq. (35) can be further calculated by

    V(θ,ϕ,r)=aH(θ,ϕ,r)[b(θ,ϕ)IM]H×UnUHn[b(θ,ϕ)IM]a(θ,ϕ,r)=aH(θ,ϕ,r)Q(θ,ϕ)a(θ,ϕ,r) (36)

    where Q(θ,ϕ)=[b(θ,ϕ)IM]HUnUHn[b(θ,ϕ)IM],

    Eq. (36) can be transformed into a quadratic programming problem. To avoid a(θ,ϕ,r)=0M, we add a constraint eH1a(θ,ϕ,r)=1, where e1 denotes unit vector. As a result, the quadratic programming problem can be redefined as

    {min (37)

    The penalty function can be constructed as

    \begin{split} L(\theta ,\phi ,r) =& {{\boldsymbol{a}}^{\rm{H}}}(\theta ,\phi ,r){\boldsymbol{Q}}(\theta ,\phi ){\boldsymbol{a}}(\theta ,\phi ,r) \\ & - \mu \left({\boldsymbol{e}}_1^{\text{H}}{\boldsymbol{a}}(\theta ,\phi ,r) - 1\right) \\ \end{split} (38)

    where \mu is a constant, because {\boldsymbol{a}}\left( {\theta ,\phi ,r} \right) = {\boldsymbol{a}}\left( {\theta ,\phi } \right) \odot {\boldsymbol{a}}\left( r \right), so we can obtain

    \begin{split} \frac{{\partial L(\theta ,\phi ,r)}}{{\partial {\boldsymbol{a}}(r)}} =& 2{\rm{diag}}\left\{ {{\boldsymbol{a}}(\theta ,\phi )} \right\}{\boldsymbol{Q}}(\theta ,\phi ){\boldsymbol{a}}(\theta ,\phi ,r) \\ & - \mu {\rm{diag}}\left\{ {{\boldsymbol{a}}(\theta ,\phi )} \right\}{\boldsymbol{e}}_{\boldsymbol{1}}^{} \end{split} (39)

    where {\rm{diag}}( \cdot ) denotes diagonalization.

    And then let \dfrac{{\partial L(\theta ,\phi ,r)}}{{\partial {\boldsymbol{a}}(r)}} = 0, we can get

    {\boldsymbol{a}}\left( r \right) = \varsigma {{\boldsymbol{Q}}^{ - 1}}(\theta ,\phi ){\boldsymbol{e}}_1^{}./{\boldsymbol{a}}(\theta ,\phi ) (40)

    where \varsigma is a constant, ./ denotes the division of the corresponding elements, which is opposite of Hadamard product. Substituting the constraint {\boldsymbol{e}}_1^{\rm{H}}{\boldsymbol{a}}(\theta ,\phi ,r) = 1 into {\boldsymbol{a}}\left( r \right) , we can obtain \varsigma = 1/({\boldsymbol{e}}_1^{\rm{H}}{{\boldsymbol{Q}}^{ - 1}} \cdot(\theta ,\phi ){\boldsymbol{e}}_1 ), then {\boldsymbol{a}}\left( r \right) can be expressed as

    {\boldsymbol{a}}\left( r \right) = \frac{{{{\boldsymbol{Q}}^{ - 1}}\left( {\theta ,\phi } \right){{\boldsymbol{e}}_1}}}{{{\boldsymbol{e}}_1^{\rm{H}}{{\boldsymbol{Q}}^{ - 1}}\left( {\theta ,\phi } \right){{\boldsymbol{e}}_1}}}./{\boldsymbol{a}}\left( {\theta ,\phi } \right) (41)

    Substituting {\boldsymbol{a}}\left( r \right) into Eq. (37), the target azimuths and elevations can be estimated by searching two-dimensional azimuth-elevation spectrum,

    \begin{split} \hfill \lt \hat \theta ,\hat \phi \gt =& {\text{arg}}\mathop {\min }\limits_{\theta ,\phi } \frac{1}{{{\boldsymbol{e}}_1^{\text{H}}{{\boldsymbol{Q}}^{ - 1}}(\theta ,\phi ){{\boldsymbol{e}}_{\boldsymbol{1}}}}} \\ =& {\text{arg}}\mathop {\max }\limits_{\theta ,\phi } {\boldsymbol{e}}_1^{\text{H}}{{\boldsymbol{Q}}^{ - 1}}(\theta ,\phi ){{\boldsymbol{e}}_{\boldsymbol{1}}} \end{split} (42)

    Given azimuth-elevation estimations obtained by mapping the L peak points, the range information can be obtained by searching range-dimensional spectrum,

    P\left({\hat \theta _i},{\hat \phi _i},r\right){\text{ }} = \frac{1}{{{\boldsymbol{a}}_{t,r}^{\rm{H}}\left({{\hat \theta }_i},{{\hat \phi }_i},r\right){{\boldsymbol{U}}_n}{\boldsymbol{U}}_n^{\rm{H}}{{\boldsymbol{a}}_{t,r}}\left({{\hat \theta }_i},{{\hat \phi }_i},r\right)}} (43)

    For conformal array, different array layouts produce different element patterns. We select the semi conical conformal array which is shown in Fig. 2 as the receiving array for the following simulation.

    Figure  2.  Conformal FDA-MIMO semi conical receiving array

    The simulation parameters are provided as follows: M = 10,N = 7,{f_1} = 10\;{\rm{GHz}},\Delta f = 3\;{\rm{kHz}}, d = \lambda /2 = c/2{f_1} and c = 3 \times {10^8}\;{\rm{m}}/{\rm{s}}.

    We first analyze the computational complexity of the algorithms in respect of the calculation of covariance matrix, the eigenvalue decomposition of the matrix and the spectral search. The main complexity of the MUISC algorithm and our proposed RD-MUISC algorithm are respectively as

    O\left(KL{({MN})^2} + 4/3{({MN})^{\text{3}}}{{ + L}}{\eta _1}{\eta _2}{\eta _3}{({MN})^2} \right) (44)
    O\left(KL{({MN})^2} + 4/3{({MN})^{\text{3}}}{{ + L}}{\eta _1}{\eta _2}{({MN})^2} + L{\eta _3}{({MN})^2}\right) (45)

    Where K and L denote snapshot number and signal sources number, {\eta _1},{\eta _2} and {\eta _3} represent search number in three-dimensional parameter \theta ,\phi ,r , respectively.

    From Eq. (44) and Eq. (45), we can see that the main complexity reduction of the RD-MUSIC algorithm lies in the calculation of the spectral search function. With the increase of the search accuracy, the complexity reduction is more significant.

    The computational complexity of algorithms is compared in Fig. 3. It can be seen from Fig. 3 that the difference of computational complexity between the two algorithms gradually increases with the increase of search accuracy. In the case of high accuracy, the computational efficiency of RD-MUSIC algorithm can reach more than {10^3} times of the traditional MUSIC algorithm. The simulation results show that RD-MUSIC algorithm has advantage in computing efficiency for conformal FDA-MIMO.

    Figure  3.  Comparison of computational complexity under different scan spacing

    In order to illustrate the effectiveness of the RD-MUSIC algorithm for a single target which is located at ({30^\circ },{20^\circ },10\;{\rm{km}}), we first give the parameter estimation probability of success with 1000 times Monte Carlo simulation, as shown in Fig. 4, the criterion of successful estimation is defined as the absolute difference between the estimation value and the actual value is less than a designed threshold \varGamma . More specifically, the criterion is \left| {\hat \theta - \theta } \right| < {\varGamma _\theta },\left| {\hat \phi - \phi } \right| < {\varGamma _\phi },\left| {\hat r - r} \right| < {\varGamma _r} , and suppose {\varGamma _\theta } = \varGamma \times {1^\circ },{\varGamma _\phi } = \varGamma \times {1^\circ },{\varGamma _r} = \varGamma \times 100\;{\rm{m}}, in the simulation, as well as the search paces are set as \left[ {{{0.05}^\circ },{{0.05}^\circ },0.05\;{\rm{km}}} \right], respectively. From Fig. 4, we can see that the probability of success gets higher as \varGamma gets bigger, which is consistent with expected.

    Figure  4.  The parameter estimation probability of RD-MUSIC algorithm with different thresholds

    Then, we consider the single target parameter estimation performance, Fig. 5 shows the RMSE of different algorithms with the increase of SNR under 200 snapshots condition, and Fig. 6 demonstrates the RMSE of different algorithms with the increase of snapshot number when SNR=0 dB. As shown in Fig. 5 and Fig. 6, the RMSEs of conformal FDA-MIMO gradually descend with the increasing of SNRs and snapshots, respectively. At the same time, the performance of traditional algorithm is slightly higher than RD-MUSIC algorithm. When the number of snapshots is more than 200, the difference of RMSEs is less than {10^{ - 1}} . Therefore, the performance loss of RD-MUSIC algorithm is acceptable compared with the improved computational speed. Note that, here we set 100 times Monte Carlo simulation to avoid running too long.

    Figure  5.  The RMSE versus snapshot for single target case
    Figure  6.  The RMSE versus SNR for two targets case

    Without loss of generality, we finally consider two targets which are located at ({30^\circ },{20^\circ }, 10\;{\rm{km}}) and ({30^\circ },{20^\circ },12\;{\rm{km}}), respectively, the remaining parameters are the same as single target case. Fig. 7 and Fig. 8 respectively show the RMSE of different algorithms with the increase of SNR and snapshot number in the case of two targets.

    Figure  7.  The RMSE versus snapshot for two targets case
    Figure  8.  The RMSE versus snapshot for two targets case

    It can be seen from Fig. 7 that the RMSE curve trend of angle estimation is consistent with that of single target case. The performance of traditional MUSIC algorithm is slightly better than that of RD-MUSIC algorithm. In the range dimension, the performance of traditional algorithm hardly changes with SNR, and RD-MUSIC algorithm is obviously better than traditional MUSIC algorithm. The proposed RD-MUSIC algorithm first estimates the angles, and then estimates the multiple peaks from range-dimensional spectrum, which avoids the ambiguity in the three-dimensional spectral search. Therefore, the RD-MUSIC algorithm has better range resolution for multiple targets estimation.

    In this paper, a conformal FDA-MIMO radar is first established, and the corresponding signal receiving mathematical model is formulated. In order to avoid the computational complexity caused by three-dimensional parameter search of MUSIC algorithm, we propose a RD-MUSIC algorithm by solving a quadratic programming problem. Simulation results show that the RD-MUSIC algorithm has comparative angle estimation performance with that of traditional MUSIC algorithm while greatly reducing the computation time. And the RD-MUSIC algorithm has better range estimation performance for multiple targets.

  • 图  1  FRFT对LFM信号检测原理框图

    Figure  1.  Diagram of LFM signal detection via FRFT

    图  2  FRFT域动目标检测原理框图[6]

    Figure  2.  Flowchart of moving target detection in FRFT domain[6]

    图  3  海上机动目标的距离和多普勒徙动(X波段CSIR雷达数据)

    Figure  3.  Range and Doppler migrations of marine maneuvering target (X-band CISR data)

    图  4  基于长时间相参积累的高速高机动目标检测方法

    Figure  4.  High-speed and maneuvering target detection based on long-time coherent integration

    图  5  利用目标加速度信息的长时间相参积累检测方法(S波段雷达数据)[13]

    Figure  5.  Long-time coherent integration-based detection method using acceleration of target (S-band radar data)[13]

    图  6  典型海上微动目标回波特性

    Figure  6.  Properties of some typical marine targets with micromotion

    图  7  基于MCA海上微动目标检测和特征提取处理结果(S波段雷达数据,Pfa=10–4)[42]

    Figure  7.  Detection and signature extraction of marine micromotion target via MCA (S-band radar data, Pfa=10–4)[42]

    图  8  FFT与SFT的运算量对比分析(美国MIT实验室)

    Figure  8.  Comparison of computation cost between FFT and SFT (MIT Laboratory)

    图  9  传统时频分析和稀疏时频分析技术的人体运动目标回波分析结果对比

    Figure  9.  Comparison of human movement analysis between traditional TFD and STFD

    图  10  基于STFD的海上动目标检测结果对比(X波段CSIR雷达数据TFC17_006,切面图,Pfa=10–4)

    Figure  10.  Marine moving target detection comparisons via different STFDs (X-band CSIR datasets TFC17_006, slice plot, Pfa=10–4)

    表  1  检测性能和计算时间对比(仿真机动目标+TFC17_006海杂波,采样点1024, Pfa=10–4)

    Table  1.   Comparison of detection performance and computational burden (Simulated moving target+TFC17_006 sea clutter, sampling number 1024, Pfa=10–4)

    检测方法 MTD SFT FRFT SFRFT FRAF SFRAF
    稀疏信号分量 13 10 2
    Pd (SCR= –5 dB) 62.47% 68.35% 68.74% 70.21% 85.69% 89.35%
    计算时间* (ms) 4.69 5.73 12.54 8.92 14.61 10.52
    “*”:计算机配置:Intel Core i7-4790 3.6 GHz CPU; 16 G RAM; Matlab R2014a,计算时间为算法1次运算时间
    下载: 导出CSV
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  • 收稿日期:  2016-09-29
  • 修回日期:  2017-02-21
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