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CN113325406B - A Passive Localization Method Based on Regularized Constrained Weighted Least Squares - Google Patents

A Passive Localization Method Based on Regularized Constrained Weighted Least Squares Download PDF

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CN113325406B
CN113325406B CN202110565144.1A CN202110565144A CN113325406B CN 113325406 B CN113325406 B CN 113325406B CN 202110565144 A CN202110565144 A CN 202110565144A CN 113325406 B CN113325406 B CN 113325406B
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国强
李文韬
王亚妮
戚连刚
乔勒纳果勒·列昂尼德
尼古拉·卡留日内
刘立超
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Abstract

The invention provides a regularized constraint weighted least square-based passive positioning method. The method comprises two steps, wherein a positioning model based on an RCTLS (global positioning system) idea is established for a TDOA/FDOA positioning problem in a first step, regularization parameters are solved based on a criterion of minimizing a mean square error, and then a closed-type analytic solution of the model is given through mathematical deduction; and the second step is to establish an equation about the estimation error of the first step by using constraint conditions, then solve the equation, and finally correct the estimation result of the first step by using the solved equation. The method can improve the positioning precision of the positioning method based on the CTLS model, and the performance is more stable under the condition that the coefficient matrix is in a pathological state.

Description

一种基于正则化约束加权最小二乘的无源定位方法A Passive Location Method Based on Regularized Constrained Weighted Least Squares

技术领域Technical Field

本发明涉及无源雷达定位领域,可在军民领域对运动目标的位置和速度进行实时的估计,具体涉及一种基于正则化约束加权最小二乘的TDOA/FDOA无源定位方法。The present invention relates to the field of passive radar positioning and can be used to estimate the position and speed of a moving target in real time in military and civilian fields, and in particular to a TDOA/FDOA passive positioning method based on regularized constrained weighted least squares.

背景技术Background Art

目前多站无源定位技术已广泛地应用于各种军民领域,如传感器网络、雷达、导航等。多站无源定位技术可以利用的观测量主要包括到达角(Angel of Arrival,AOA)、到达时间差(Time Difference of Arrival,TDOA)、到达频率差(Frequency Difference ofArrival,FDOA)等。At present, multi-station passive positioning technology has been widely used in various military and civilian fields, such as sensor networks, radar, navigation, etc. The observations that can be used in multi-station passive positioning technology mainly include angle of arrival (AOA), time difference of arrival (TDOA), frequency difference of arrival (FDOA), etc.

联合不同测量参数的定位体制可以融合不同参数的优势,在一定程度上提高定位精度,而联合TDOA和FDOA的定位体制由于可同时对目标的位置和速度进行估计,得到了广泛德研究。近些年来,针对基于TDOA/FDOA的定位问题的算法相继提出,其中包括两步加权最小二乘法(Two-Stage Weighted Least Squares,TSWLS)、约束总体最小二乘(Constrained Total Least Squares,CTLS)等。但由于噪声的干扰、接收站和目标位置的分布以及接收站个数对系数矩阵的影响,以上这些基于CWLS、CTLS模型的方法中的系数矩阵在实际应用中可能会出现病态的问题。The positioning system combining different measurement parameters can integrate the advantages of different parameters and improve the positioning accuracy to a certain extent. The positioning system combining TDOA and FDOA has been widely studied because it can estimate the position and velocity of the target at the same time. In recent years, algorithms for positioning problems based on TDOA/FDOA have been proposed one after another, including Two-Stage Weighted Least Squares (TSWLS) and Constrained Total Least Squares (CTLS). However, due to the interference of noise, the distribution of receiving stations and target positions, and the influence of the number of receiving stations on the coefficient matrix, the coefficient matrices in the above methods based on CWLS and CTLS models may have ill-conditioned problems in practical applications.

发明内容Summary of the invention

本申请发明针对TDOA/FDOA无源定位问题中的系数矩阵病态问题,基于RCTLS的思想提出了两步正则化约束最小二乘方法(Two-Stage Regularized Constrained TotalLeast Squares,TRCTLS),这种方法在CTLS模型的基础上引入了正则化参数,通过合理地选取正则化参数来提高定位的均方根误差以及抑制系数矩阵的病态性。The present invention aims at the ill-posed problem of coefficient matrix in TDOA/FDOA passive positioning problem, and proposes a two-stage regularized constrained least squares method (Two-Stage Regularized Constrained TotalLeast Squares, TRCTLS) based on the idea of RCTLS. This method introduces a regularization parameter on the basis of the CTLS model, and improves the root mean square error of positioning and suppresses the ill-posed nature of the coefficient matrix by reasonably selecting the regularization parameter.

本发明的目的是这样实现的:本发明的步骤如下:The object of the present invention is achieved in that the steps of the present invention are as follows:

步骤1:根据测得的TDOA和FDOA信息建立定位方程;Step 1: Establish the positioning equation based on the measured TDOA and FDOA information;

步骤2:基于RCTLS的思想对定位方程进行求解,得到一个含有正则化参数的闭式解;Step 2: Solve the positioning equation based on the idea of RCTLS to obtain a closed-form solution containing regularization parameters;

步骤3:基于最小化均方误差的准则对第二步中的正则化参数进行求解;Step 3: Solve the regularization parameter in the second step based on the criterion of minimizing the mean square error;

步骤4:利用约束条件建立起关于第一步估计误差的方程后进行求得一个包含正则化参数的解;Step 4: Use the constraints to establish an equation for the error in the first step and then find a solution that includes the regularization parameter;

步骤5:同样基于最小化均方误差的准则对步骤4中所得解包含的正则化参数进行求解,之后利用第四步中所得到的解对第二步中得到的结果进行修正以得到最终的解。Step 5: Also based on the criterion of minimizing the mean square error, the regularization parameter contained in the solution obtained in step 4 is solved, and then the result obtained in step 2 is corrected using the solution obtained in step 4 to obtain the final solution.

本发明还包括这样一些结构特征:The present invention also includes such structural features:

1.步骤1中得到的基于TDOA/FDOA的定位方程为:1. The positioning equation based on TDOA/FDOA obtained in step 1 is:

Figure BDA0003080670390000021
Figure BDA0003080670390000021

式中ri1为所测得的主站与辅站之间距离目标的距离差,si

Figure BDA0003080670390000022
为接收站的位置和速度坐标,uo为目标的位置和速度坐标,εt=BΔr,为TDOA方程的误差项,
Figure BDA0003080670390000023
为FDOA方程的误差项,其中
Figure BDA0003080670390000024
Where r i1 is the distance difference between the primary station and the secondary station from the target, s i and
Figure BDA0003080670390000022
are the position and velocity coordinates of the receiving station, u o are the position and velocity coordinates of the target, ε t = BΔr, is the error term of the TDOA equation,
Figure BDA0003080670390000023
is the error term of the FDOA equation, where
Figure BDA0003080670390000024

2.步骤2具体为:2. Step 2 is as follows:

构造辅助变量

Figure BDA0003080670390000025
根据CTLS方法将基于TDOA/FDOA的定位模型表示为如下形式:Constructing auxiliary variables
Figure BDA0003080670390000025
According to the CTLS method, the positioning model based on TDOA/FDOA is expressed as follows:

(A+ΔA)θ1=(b+Δb)(A+ΔA)θ 1 =(b+Δb)

式中:Where:

Figure BDA0003080670390000026
Figure BDA0003080670390000026

Figure BDA0003080670390000027
Figure BDA0003080670390000027

Figure BDA0003080670390000028
Figure BDA0003080670390000028

Figure BDA0003080670390000029
Figure BDA0003080670390000029

其中O(M-1)×2N为(M-1)×2N的零矩阵,0为3×1的零向量。利用RCTLS的思想对该方程进行求解即可得到一个含有正则化参数的闭式解:Among them, O (M-1)×2N is a (M-1)×2N zero matrix, and 0 is a 3×1 zero vector. Solving this equation using the idea of RCTLS can obtain a closed-form solution containing the regularization parameter:

Figure BDA00030806703900000210
Figure BDA00030806703900000210

3.步骤3具体为:3. Step 3 is as follows:

该步骤主要是对步骤2所得解中的正则化参数进行求解,通过数学推导可将第一步估计中估计误差的均方误差表示为:This step is mainly to solve the regularization parameter in the solution obtained in step 2. Through mathematical derivation, the mean square error of the estimation error in the first step of estimation can be expressed as:

Figure BDA0003080670390000031
Figure BDA0003080670390000031

则基于最小化均方误差的准则对上式进行求解可得正则化参数为:Then, based on the criterion of minimizing the mean square error, the regularization parameter can be solved as follows:

Figure BDA0003080670390000032
Figure BDA0003080670390000032

步骤4具体为:Step 4 is as follows:

令步骤2中的估计误差分别为Δu=u1-uo

Figure BDA0003080670390000033
Figure BDA0003080670390000034
将步骤2中辅助变量的真实值
Figure BDA0003080670390000035
Figure BDA0003080670390000036
在u1
Figure BDA0003080670390000037
处进行一阶泰勒展开可得:Let the estimated errors in step 2 be Δu=u 1 -u o ,
Figure BDA0003080670390000033
make
Figure BDA0003080670390000034
The true value of the auxiliary variable in step 2
Figure BDA0003080670390000035
and
Figure BDA0003080670390000036
In u 1 and
Figure BDA0003080670390000037
Performing a first-order Taylor expansion at gives:

Figure BDA0003080670390000038
Figure BDA0003080670390000038

Figure BDA0003080670390000039
Figure BDA0003080670390000039

将上式以及式Δu=u1-uo

Figure BDA00030806703900000310
代入步骤2中的定位模型可得:Substituting the above formula and the formula Δu=u 1 -u o ,
Figure BDA00030806703900000310
Substituting into the positioning model in step 2, we get:

(M+ΔM)θ2=N+ΔN(M+ΔM)θ 2 =N+ΔN

式中:Where:

Figure BDA00030806703900000311
Figure BDA00030806703900000311

Figure BDA00030806703900000312
Figure BDA00030806703900000312

Figure BDA00030806703900000313
Figure BDA00030806703900000313

Figure BDA0003080670390000041
Figure BDA0003080670390000041

同样基于RCTLS的思想对该方程进行求解可得:Based on the idea of RCTLS, we can solve the equation:

Figure BDA0003080670390000042
Figure BDA0003080670390000042

同步骤3的思想一样,步骤5也是基于最小化均方误差的准则对步骤4中所得解的正则化参数进行估计。Similar to the idea of step 3, step 5 also estimates the regularization parameter of the solution obtained in step 4 based on the criterion of minimizing the mean square error.

与现有技术相比,本发明的有益效果是:通过理论推导和仿真实验均表明本发明的这种方法通过合理选择正则化参数可以在CTLS方法的基础上进一步降低算法的均方根误差(Root Mean Square Error,RMSE),同时在系数矩阵出现病态时的定位性能也更加稳定。Compared with the prior art, the beneficial effects of the present invention are as follows: theoretical derivation and simulation experiments show that the method of the present invention can further reduce the root mean square error (RMSE) of the algorithm on the basis of the CTLS method by reasonably selecting the regularization parameter, and the positioning performance is also more stable when the coefficient matrix is ill-conditioned.

附图说明BRIEF DESCRIPTION OF THE DRAWINGS

图1是接收站对运动目标进行定位的模型;Figure 1 is a model of a receiving station positioning a moving target;

图2是本发明的实现流程图;Fig. 2 is an implementation flow chart of the present invention;

图3是三种定位场景中接收站以及目标位置分布;Figure 3 shows the distribution of receiving stations and target locations in three positioning scenarios;

图4是场景一中三种方法的位置估计均方根误差;Figure 4 shows the root mean square error of position estimation of the three methods in scenario 1;

图5是场景一中三种方法的速度估计均方根误差;Figure 5 shows the root mean square error of velocity estimation of the three methods in scenario 1;

图6是场景二中三种方法的位置估计均方根误差;Figure 6 shows the root mean square error of position estimation for the three methods in scenario 2;

图7是场景二中三种方法的速度估计均方根误差;Figure 7 shows the root mean square error of speed estimation of the three methods in scenario 2;

图8是场景三中三种方法的位置估计均方根误差;Figure 8 shows the root mean square error of position estimation of the three methods in scenario 3;

图9是场景三中三种方法的速度估计均方根误差。Figure 9 shows the root mean square error of speed estimation of the three methods in scenario three.

具体实施方式DETAILED DESCRIPTION

下面结合附图与具体实施方式对本发明作进一步详细描述。The present invention is further described in detail below in conjunction with the accompanying drawings and specific embodiments.

一种基于正则化约束总体最小二乘的定位方法,具体包括:A positioning method based on regularized constrained total least squares, specifically comprising:

(1)如图1所示,在三维空间中利用M个接收站对运动的目标辐射源进行定位,目标辐射源的位置和速度分别为uo=[x,y,z]T

Figure BDA0003080670390000043
第i个接收站的位置和速度分别为si=[xi,yi,zi]T
Figure BDA0003080670390000044
则接收站与目标辐射源之间的真实距离可以表示为:(1) As shown in Figure 1, M receiving stations are used to locate the moving target radiation source in three-dimensional space. The position and velocity of the target radiation source are u o = [x, y, z] T ,
Figure BDA0003080670390000043
The position and velocity of the i-th receiving station are s i = [x i , y i , z i ] T ,
Figure BDA0003080670390000044
Then the actual distance between the receiving station and the target radiation source can be expressed as:

Figure BDA0003080670390000045
Figure BDA0003080670390000045

选取其中任意一个接收站为主站,编号为1,其余的接收站均为辅站,则主站与各辅站之间的真实距离差为:Select any one of the receiving stations as the main station, numbered 1, and the rest of the receiving stations as auxiliary stations. The actual distance difference between the main station and each auxiliary station is:

Figure BDA0003080670390000051
Figure BDA0003080670390000051

其中

Figure BDA0003080670390000052
由真实的TDOA数据计算得到,其向量形式可记为
Figure BDA0003080670390000053
由上述可得基于TDOA的定位方程:in
Figure BDA0003080670390000052
Calculated from real TDOA data, its vector form can be expressed as
Figure BDA0003080670390000053
From the above, the positioning equation based on TDOA can be obtained:

Figure BDA0003080670390000054
Figure BDA0003080670390000054

Figure BDA0003080670390000055
的定义式进行求导可得接收站与目标辐射源之间真实的距离变化率的定义式:right
Figure BDA0003080670390000055
By taking the derivative of the definition, we can get the definition of the actual rate of change of distance between the receiving station and the target radiation source:

Figure BDA0003080670390000056
Figure BDA0003080670390000056

对TDOA方程求时间导数可得基于FDOA的定位方程:Taking the time derivative of the TDOA equation gives the positioning equation based on FDOA:

Figure BDA0003080670390000057
Figure BDA0003080670390000057

其中

Figure BDA0003080670390000058
是由真实的FDOA信息推导出的真实距离差变化率,其向量形式可记为
Figure BDA0003080670390000059
假设利用实际测量得到的TDOA和FDOA数据得到的距离差向量和距离差变化率向量分别为r=[r21,r31,…,rM1]T
Figure BDA00030806703900000510
可将其描述为真实值与噪声值相加的形式:in
Figure BDA0003080670390000058
is the rate of change of the actual distance difference derived from the actual FDOA information, and its vector form can be expressed as
Figure BDA0003080670390000059
Assume that the distance difference vector and the distance difference change rate vector obtained by using the TDOA and FDOA data obtained by actual measurement are r = [r 21 , r 31 , …, r M1 ] T and
Figure BDA00030806703900000510
It can be described as the sum of the true value and the noise value:

r=ro+Δr=ro+cΔtr= ro +Δr= ro +cΔt

Figure BDA00030806703900000511
Figure BDA00030806703900000511

其中TDOA和FDOA测量数据中所包含的测量噪声分别为Δr=[Δr21,Δr31,…,ΔrM1]T以及

Figure BDA00030806703900000512
假设它们服从均值为零的高斯分布,则其协方差矩阵为:The measurement noises included in the TDOA and FDOA measurement data are Δr = [Δr 21 , Δr 31 , …, Δr M1 ] T and
Figure BDA00030806703900000512
Assuming they follow a Gaussian distribution with mean zero, their covariance matrix is:

Figure BDA00030806703900000513
Figure BDA00030806703900000513

将包含噪声的TDOA测量值r=ro+Δr和FDOA测量值

Figure BDA00030806703900000514
代入TDOA方程和FDOA方程中并忽略二阶误差项可以得到包含误差项的TDOA/FDOA方程:The TDOA measurement value r = r o + Δr and the FDOA measurement value containing noise are
Figure BDA00030806703900000514
Substituting into the TDOA equation and FDOA equation and ignoring the second-order error term, we can obtain the TDOA/FDOA equation including the error term:

Figure BDA00030806703900000515
Figure BDA00030806703900000515

其中εt=BΔr,为TDOA方程的误差项,

Figure BDA00030806703900000516
为FDOA方程的误差项,
Figure BDA00030806703900000517
Where ε t = BΔr, is the error term of the TDOA equation,
Figure BDA00030806703900000516
is the error term of the FDOA equation,
Figure BDA00030806703900000517

(2)构造辅助变量

Figure BDA00030806703900000518
首先根据CTLS模型将包含误差项的定位方程表示为矩阵形式:(2) Constructing auxiliary variables
Figure BDA00030806703900000518
First, according to the CTLS model, the positioning equation containing the error term is expressed in matrix form:

(A+ΔA)θ1=(b+Δb)(A+ΔA)θ 1 =(b+Δb)

式中:Where:

Figure BDA0003080670390000061
Figure BDA0003080670390000061

Figure BDA0003080670390000062
Figure BDA0003080670390000062

Figure BDA0003080670390000063
Figure BDA0003080670390000063

Figure BDA0003080670390000064
Figure BDA0003080670390000064

其中O(M-1)×2N为(M-1)×2N的零矩阵,0为3×1的零向量。从矩阵A的表达式中可以看出,接收站和目标位置的不合理分布、噪声的干扰均可能会导致矩阵A出现病态,比如当接收站的坐标在x轴上比较接近时,那么此时矩阵A的条件数会明显增加,矩阵将出现病态,从而导致定位结果对噪声的敏感性增加。而引入正则化参数是一种有效抑制矩阵病态问题的手段。令噪声矩阵

Figure BDA0003080670390000065
可以看出ΔA和Δb中的噪声是具有相关性的,可以将矩阵ΔA和Δb表示为:Among them, O (M-1)×2N is a zero matrix of (M-1)×2N, and 0 is a 3×1 zero vector. From the expression of matrix A, it can be seen that the unreasonable distribution of receiving stations and target positions and the interference of noise may cause matrix A to become ill-conditioned. For example, when the coordinates of the receiving stations are close on the x-axis, the condition number of matrix A will increase significantly, and the matrix will become ill-conditioned, resulting in increased sensitivity of positioning results to noise. Introducing regularization parameters is an effective means to suppress the ill-conditioned problem of matrices. Let the noise matrix
Figure BDA0003080670390000065
It can be seen that the noise in ΔA and Δb is correlated, and the matrices ΔA and Δb can be expressed as:

ΔA=[F1n,F2n,…,Fln]ΔA=[F 1 n, F 2 n,..., F l n]

Δb=Fl+1nΔb=F l+1 n

其中l为矩阵ΔA的列数(l=8),F1到F9的值可以表示为:Where l is the number of columns of the matrix ΔA (l=8), the values of F1 to F9 can be expressed as:

Fi=O2(M-1)×2(M-1)(i=1,2,…,6)F i =O 2(M-1)×2(M-1) (i=1,2,…,6)

F7=-2×I2(M-1)×2(M-1)F 7 = -2 × I 2 (M-1) × 2 (M-1 )

Figure BDA0003080670390000066
Figure BDA0003080670390000066

Figure BDA0003080670390000067
Figure BDA0003080670390000067

式中:∑11=∑22=diag(r21,r31,…,rM1)、

Figure BDA0003080670390000068
考虑到n中各项误差具有相关性且有着不同的方差,对其进行白化处理。令Q=E[nnT],对Q做Cholesky分解可得Q=PPT,则n的白化向量为σ=P-1n,同时可以得到ΔA=[G1σ,G2σ,…,Glσ]、Δb=Fl+1n,其中Gi=FiP,基于RCTLS思想可将定位方程转换为如下形式:Where: ∑ 11 =∑ 22 =diag(r 21 ,r 31 ,…,r M1 ),
Figure BDA0003080670390000068
Considering that the errors in n are correlated and have different variances, they are whitened. Let Q = E[nn T ], and perform Cholesky decomposition on Q to obtain Q = PP T , then the whitened vector of n is σ = P -1 n, and at the same time, we can obtain ΔA = [G 1 σ, G 2 σ, ..., G l σ], Δb = F l+1 n, where G i = F i P. Based on the RCTLS idea, the positioning equation can be converted into the following form:

min(‖σ‖21‖θ12)min(‖σ‖ 21 ‖θ 12 )

Figure BDA0003080670390000071
Figure BDA0003080670390000071

经过简单的数学运算,上式可转换为如下函数的求极小值问题:After simple mathematical operations, the above formula can be converted into the problem of finding the minimum value of the following function:

Figure BDA0003080670390000072
Figure BDA0003080670390000072

对上式求导后可得:After taking the derivative of the above formula, we can get:

Figure BDA0003080670390000073
Figure BDA0003080670390000073

式中

Figure BDA0003080670390000074
进而对该式进行求解可得方程的RCTLS解:In the formula
Figure BDA0003080670390000074
Then, the RCTLS solution of the equation can be obtained by solving the equation:

Figure BDA0003080670390000075
Figure BDA0003080670390000075

(3)上一步得到的解并未考虑约束条件,因此在这一步中将利用约束条件重新构造一组方程以完成对第一步估计值的修正。假设目标的真实位置和速度为uo

Figure BDA0003080670390000076
从第一步得到的目标估计位置和速度分别为u1
Figure BDA0003080670390000077
则第一步的估计误差为Δu=u1-uo
Figure BDA0003080670390000078
Figure BDA0003080670390000079
将第一步中辅助变量的真实值
Figure BDA00030806703900000710
Figure BDA00030806703900000711
在u1
Figure BDA00030806703900000712
处进行一阶泰勒展开可得:(3) The solution obtained in the previous step does not take into account the constraints, so in this step, we will use the constraints to reconstruct a set of equations to correct the estimated values in the first step. Assume that the actual position and velocity of the target are u o and
Figure BDA0003080670390000076
The estimated position and velocity of the target obtained from the first step are u 1 and
Figure BDA0003080670390000077
Then the estimation error of the first step is Δu=u 1 -u o ,
Figure BDA0003080670390000078
make
Figure BDA0003080670390000079
The true value of the auxiliary variable in the first step
Figure BDA00030806703900000710
and
Figure BDA00030806703900000711
In u 1 and
Figure BDA00030806703900000712
Performing a first-order Taylor expansion at gives:

Figure BDA00030806703900000713
Figure BDA00030806703900000713

Figure BDA00030806703900000714
Figure BDA00030806703900000714

记第一步得到的辅助变量估计值为r1

Figure BDA00030806703900000715
则α和β的表达式为:Let the estimated values of the auxiliary variables obtained in the first step be r 1 and
Figure BDA00030806703900000715
Then the expressions of α and β are:

α=(u1-s1)/r1 α=(u 1 −s 1 )/r 1

Figure BDA00030806703900000716
Figure BDA00030806703900000716

将Δu=u1-uo

Figure BDA00030806703900000717
以及
Figure BDA00030806703900000718
Figure BDA00030806703900000719
的泰勒展开式代入定位方程中可得:Δu=u 1 -u o ,
Figure BDA00030806703900000717
as well as
Figure BDA00030806703900000718
and
Figure BDA00030806703900000719
Substituting the Taylor expansion of into the positioning equation yields:

(M+ΔM)θ2=N+ΔN(M+ΔM)θ 2 =N+ΔN

式中:Where:

Figure BDA00030806703900000720
Figure BDA00030806703900000720

Figure BDA00030806703900000721
Figure BDA00030806703900000721

Figure BDA0003080670390000081
Figure BDA0003080670390000081

Figure BDA0003080670390000082
Figure BDA0003080670390000082

其中ΔM和ΔN可表示为:Where ΔM and ΔN can be expressed as:

ΔM=[U1n,U2n,…,Ukn]ΔM=[U 1 n, U 2 n,..., U k n]

ΔN=Uk+1nΔN=U k+1 n

式中k为矩阵的列数(k=6),U1,U2…Uk的具体表达式略,对n进行白化处理后可得:Where k is the number of columns of the matrix (k=6), the specific expressions of U 1 ,U 2 …U k are omitted, and after whitening n, we can get:

ΔM=[V1n,V2n,…,Vkn]ΔM=[V 1 n,V 2 n,…,V k n]

ΔN=Vk+1nΔN=V k+1 n

其中Vi=UiP,则(M+ΔM)θ2=N+ΔN可转换为如下形式:Where V i = U i P, then (M+ΔM)θ 2 = N+ΔN can be converted into the following form:

Figure BDA0003080670390000083
Figure BDA0003080670390000083

其中

Figure BDA0003080670390000084
利用第一步的RCTLS算法对上式进行求解可得:in
Figure BDA0003080670390000084
Using the first step of the RCTLS algorithm to solve the above equation, we can get:

Figure BDA0003080670390000085
Figure BDA0003080670390000085

其中

Figure BDA0003080670390000086
则目标位置和速度的最终估计值分别为
Figure BDA0003080670390000087
in
Figure BDA0003080670390000086
The final estimated values of the target position and velocity are
Figure BDA0003080670390000087

(4)需要从最小化均方误差的原则对步骤(2)和(3)中的正则化参数进行求解。首先对求解步骤(2)中的正则化参数进行求解,假设步骤(2)中的估计值

Figure BDA0003080670390000088
与真实值θ1之间的关系为:(4) It is necessary to solve the regularization parameters in steps (2) and (3) based on the principle of minimizing the mean square error. First, solve the regularization parameter in step (2). Assume that the estimated value in step (2) is
Figure BDA0003080670390000088
The relationship between the true value θ 1 is:

Figure BDA0003080670390000089
Figure BDA0003080670390000089

将上式代入函数F(θ1)的导数中可得:Substituting the above formula into the derivative of function F(θ 1 ) yields:

Figure BDA00030806703900000810
Figure BDA00030806703900000810

Figure BDA00030806703900000811
则由上式可得:make
Figure BDA00030806703900000811
From the above formula we can get:

Figure BDA00030806703900000812
Figure BDA00030806703900000812

Figure BDA0003080670390000091
可得:make
Figure BDA0003080670390000091
We can get:

Δθ1 TΔθ1=(JT1θ1 T)[(SA+λ1I8×8)-1]T(SA+λ1I8×8)-1(J+λ1θ1)Δθ 1 T Δθ 1 =(J T1 θ 1 T )[(SA+λ 1 I 8×8 ) -1 ] T (SA+λ 1 I 8×8 ) -1 (J+λ 1 θ 1 )

通常矩阵SA为满秩矩阵,则存在一个标准正交矩阵使得SA对角化:Usually the matrix SA is a full rank matrix, then there exists a standard orthogonal matrix that diagonalizes SA:

SA=PTdiag{u1,u2,…,u8}PSA=P T diag{u 1 , u 2 ,..., u 8 }P

对[(SA+λ1I8×8)-1]T(SA+λ1I8×8)-1进行特征值分解可得:Performing eigenvalue decomposition on [(SA+λ 1 I 8×8 ) -1 ] T (SA+λ 1 I 8×8 ) -1 yields:

[(SA+λ1I8×8)-1]T(SA+λ1I8×8)-1=PTDP[(SA+λ 1 I 8×8 ) -1 ] T (SA+λ 1 I 8×8 ) -1 =P T DP

式中P是8×8的标准正交矩阵,D=diag{(i11)-2,(u21)-2,…,(u81)-2}。考虑到E(J)=0,对Δθ1 TΔθ1的表达式取期望可得第一步所得估计值的均方误差为:Where P is a 8×8 standard orthogonal matrix, D=diag{(i 11 ) -2 ,(u 21 ) -2 ,…,(u 81 ) -2 }. Considering E(J)=0, taking the expected value of the expression of Δθ 1 T Δθ 1, the mean square error of the estimated value obtained in the first step is:

Figure BDA0003080670390000092
Figure BDA0003080670390000092

令C1=PJ、C2=Pθ1,则C1、C2为两个列向量。设C1=[c11,c12,…,c18]T、C2=[c21,c22,…,c28]T,则E[Δθ1 TΔθ1]可表示为:Let C 1 = PJ, C 2 = Pθ 1 , then C 1 and C 2 are two column vectors. Let C 1 = [c 11 , c 12 , … , c 18 ] T , C 2 = [c 21 , c 22 , … , c 28 ] T , then E[Δθ 1 T Δθ 1 ] can be expressed as:

Figure BDA0003080670390000093
Figure BDA0003080670390000093

可以看出第一步中利用RCTLS算法求得的结果的均方误差是关于λ1的函数,为了求得均方误差最小值对应的λ1值,对Δθ1 TΔθ1求导可得:It can be seen that the mean square error of the result obtained by the RCTLS algorithm in the first step is a function of λ 1. In order to obtain the λ 1 value corresponding to the minimum mean square error, the derivative of Δθ 1 T Δθ 1 is obtained:

Figure BDA0003080670390000094
Figure BDA0003080670390000094

对上式进行分析可得,当

Figure BDA0003080670390000095
时,
Figure BDA0003080670390000096
此时估计均方误差随λ1单调递减;当
Figure BDA0003080670390000097
时,
Figure BDA0003080670390000098
此时估计均方误差随λ1单调递增。因此可以得到λ1最小值的取值区间为
Figure BDA0003080670390000099
则本文中取极小值为:Analyzing the above formula, we can get that
Figure BDA0003080670390000095
hour,
Figure BDA0003080670390000096
At this time, the estimated mean square error decreases monotonically with λ 1 ;
Figure BDA0003080670390000097
hour,
Figure BDA0003080670390000098
At this time, the estimated mean square error increases monotonically with λ 1. Therefore, the range of the minimum value of λ 1 can be obtained as
Figure BDA0003080670390000099
The minimum value in this paper is:

Figure BDA00030806703900000910
Figure BDA00030806703900000910

同理可得到步骤(3)中λ2的取值。注意到步骤(2)的方法中Λ和

Figure BDA00030806703900000911
均含有未知数θ1,因此在实际的计算中先假设Λ=0、
Figure BDA00030806703900000912
得到初始的估计值后将其代入矩阵Λ和
Figure BDA00030806703900000913
的表达式中对Λ和
Figure BDA00030806703900000914
进行更新,之后利用新的Λ和
Figure BDA00030806703900000915
重新计算θ1,如此循环3~5次即可得到最终的θ1,同样地,在第二步对θ2进行求解时也需要进行类似的处理。Similarly, the value of λ 2 in step (3) can be obtained. Note that in the method of step (2), Λ and
Figure BDA00030806703900000911
Both contain unknown number θ 1 , so in the actual calculation, we first assume that Λ=0,
Figure BDA00030806703900000912
After obtaining the initial estimate, substitute it into the matrix Λ and
Figure BDA00030806703900000913
In the expression of
Figure BDA00030806703900000914
Update, and then use the new Λ and
Figure BDA00030806703900000915
Recalculate θ 1 , and repeat this process 3 to 5 times to obtain the final θ 1 . Similarly, similar processing is required when solving θ 2 in the second step.

为了进一步对本实施例进行说明,对算法实施了仿真分析,仿真实验在3个场景下进行,其中场景1和场景2中目标辐射源的位置和速度分别为u=[285,325,275]Tm和

Figure BDA0003080670390000101
Figure BDA0003080670390000102
场景3中目标辐射源的位置和速度为u=[50,320,110]Tm和
Figure BDA0003080670390000103
Figure BDA0003080670390000104
每个场景均设置5个接收站,3个场景中的接收站与目标的位置在三维空间中的分布如图2所示,可以看出,3个场景中的接收站的整体分布基本接近,只有场景2中有2个接收站在z轴上的坐标与场景1和场景3中略有不同,这种设置可减少不同场景中接收站的分布方式对定位精度的影响。场景1为系数矩阵并未出现病态时的定位场景,而场景2中则因为接收站在z轴上坐标接近而导致系数矩阵出现病态,场景3则是因为目标辐射源距离5个接收站的距离接近而导致系数矩阵出现病态。在3个场景中均使用均方根误差进行性能分析,使用CRLB作为衡量估计精度的标准,同时使用TSWLS方法和CTLS方法作为对比方法。In order to further illustrate this embodiment, a simulation analysis is performed on the algorithm. The simulation experiment is carried out in three scenarios, where the position and velocity of the target radiation source in scenario 1 and scenario 2 are u = [285, 325, 275] T m and
Figure BDA0003080670390000101
Figure BDA0003080670390000102
The position and velocity of the target radiation source in scene 3 are u = [50, 320, 110] T m and
Figure BDA0003080670390000103
Figure BDA0003080670390000104
Five receiving stations are set up in each scene. The distribution of the receiving stations and the positions of the targets in the three scenes in three-dimensional space is shown in Figure 2. It can be seen that the overall distribution of the receiving stations in the three scenes is basically close. Only in scene 2, the coordinates of two receiving stations on the z-axis are slightly different from those in scenes 1 and 3. This setting can reduce the impact of the distribution of receiving stations in different scenes on the positioning accuracy. Scene 1 is a positioning scene when the coefficient matrix is not ill-conditioned, while in scene 2, the coefficient matrix is ill-conditioned because the coordinates of the receiving stations on the z-axis are close. In scene 3, the coefficient matrix is ill-conditioned because the distance between the target radiation source and the five receiving stations is close. In all three scenes, the root mean square error is used for performance analysis, and CRLB is used as the standard for measuring estimation accuracy. The TSWLS method and the CTLS method are used as comparison methods.

图4和图5、图6和图7、图8和图9则分别反映了三种方法在场景一、场景二、场景三中的定位均方根误差,可以看出本发明采用的这种算法在CTLS方法的基础上降低了算法的均方根误差,提升了算法在系数矩阵出现病态问题时的稳定性。Figures 4 and 5, Figures 6 and 7, and Figures 8 and 9 respectively reflect the root mean square errors of positioning of the three methods in scenario 1, scenario 2, and scenario 3. It can be seen that the algorithm adopted in the present invention reduces the root mean square error of the algorithm on the basis of the CTLS method, and improves the stability of the algorithm when pathological problems occur in the coefficient matrix.

本领域技术人员可以理解,在本申请具体实施方式的上述方法中,各步骤的序号大小并不意味着执行顺序的先后,各步骤的执行顺序应以其功能和内在逻辑确定,而不应对本申请具体实施方式的实施过程构成任何限定。Those skilled in the art will understand that in the above method of the specific implementation mode of the present application, the serial number of each step does not mean the order of execution. The execution order of each step should be determined by its function and internal logic, and should not constitute any limitation on the implementation process of the specific implementation mode of the present application.

最后应说明的是,以上实施例仅用以描述本发明的技术方案而不是对本技术方法进行限制,本发明在应用上可以延伸为其他的修改、变化、应用和实施例,并且因此认为所有这样的修改、变化、应用、实施例都在本发明的精神和教导范围内。Finally, it should be noted that the above embodiments are only used to describe the technical solution of the present invention rather than to limit the technical method. The present invention can be extended to other modifications, changes, applications and embodiments in application, and therefore it is believed that all such modifications, changes, applications and embodiments are within the spirit and teaching scope of the present invention.

综上,本发明提出了一种基于正则化约束总体最小二乘(RCTLS)的闭式解析法。该方法分为两步,在第一步中针对TDOA/FDOA定位问题建立了基于RCTLS思想的定位模型,同时基于最小化均方误差的准则求解正则化参数,之后通过数学推导给出了该模型的闭式解析解;第二步则是利用约束条件建立起关于第一步估计误差的方程后进行求解,最后利用求得的解对第一步的估计结果进行修正。本发明的方法可以提高基于CTLS模型的定位方法的定位精度,而且在系数矩阵出现病态的情况下性能也更加稳定。In summary, the present invention proposes a closed-form analytical method based on regularized constrained total least squares (RCTLS). The method is divided into two steps. In the first step, a positioning model based on the RCTLS concept is established for the TDOA/FDOA positioning problem, and the regularization parameter is solved based on the criterion of minimizing the mean square error. Then, the closed-form analytical solution of the model is given through mathematical derivation; the second step is to use the constraints to establish the equation about the estimation error of the first step and then solve it, and finally use the obtained solution to correct the estimation result of the first step. The method of the present invention can improve the positioning accuracy of the positioning method based on the CTLS model, and the performance is more stable when the coefficient matrix is ill-conditioned.

Claims (3)

1. A passive positioning method based on regularization constraint weighted least square is characterized by comprising the following steps: the method comprises the following steps:
step one: establishing a positioning equation according to the measured TDOA and FDOA information;
step two: solving a positioning equation based on the concept of RCTLS to obtain a closed solution containing regularization parameters;
construction auxiliary variable
Figure FDA0004122316430000011
u o =[x,y,z] T
Figure FDA0004122316430000012
The position and the velocity vector of the target radiation source to be measured are respectively, wherein [. Cndot.] T Representing a transpose operation on a vector or matrix, r 1 o For the true distance of the main receiving station from the target radiation source, < >>
Figure FDA0004122316430000013
To r is 1 o Taking the distance change rate obtained by the derivative, and expressing a positioning model based on TDOA/FDOA as the following form according to the CTLS method:
(A+ΔA)θ 1 =(b+Δb)
wherein:
Figure FDA0004122316430000014
Figure FDA0004122316430000015
Figure FDA0004122316430000016
Figure FDA0004122316430000017
wherein: s is(s) i =[x i ,y i ,z i ] T
Figure FDA0004122316430000018
The position and velocity of the ith receiving station, respectively; r is (r) i1 The true distance difference between the main receiving station 1 and each auxiliary receiving station i and the target radiation source is obtained;
Figure FDA0004122316430000019
The difference value of the change rate of the distance between the main receiving station 1 and each auxiliary receiving station i is obtained; o (O) (M-1)×2N A zero matrix of (M-1) x 2N, 0 being a zero vector of 3 x 1; r= [ r ] 21 ,r 31 ,...,r M1 ] T And
Figure FDA00041223164300000110
respectively deriving a distance difference vector and a distance difference change rate vector by using TDOA and FDOA data obtained by actual measurement; Δr= [ Δr ] 21 ,Δr 31 ,...,Δr M1 ] T
Figure FDA00041223164300000111
Noise contained in TDOA and FDOA data, respectively; solving the equation by using the concept of RCTLS to obtain a closed solution containing regularization parameters:
Figure FDA00041223164300000112
wherein:
Figure FDA0004122316430000021
and->
Figure FDA0004122316430000022
Lambda is defined as an intermediate variable 1 For regularization parameters, ++>
Step three: solving the regularization parameters in the second step based on a criterion of minimizing the mean square error;
step four: establishing an equation about the estimation error of the first step by using constraint conditions, and then solving a solution containing regularization parameters;
let the estimation errors in the second step be Δu=u, respectively 1 -u o
Figure FDA0004122316430000023
Let->
Figure FDA0004122316430000024
The true position and velocity of the target is u o And->
Figure FDA0004122316430000025
The estimated position and velocity of the target obtained from the first step are u 1 And->
Figure FDA0004122316430000026
The true value of the auxiliary variable in the second step +.>
Figure FDA0004122316430000027
And->
Figure FDA0004122316430000028
In u 1 And->
Figure FDA0004122316430000029
The first-order Taylor expansion is carried out:
Figure FDA00041223164300000210
Figure FDA00041223164300000211
the above formula and formula Δu=u 1 -u o
Figure FDA00041223164300000212
Substituting the positioning model in the step 2 to obtain:
(M+ΔM)θ 2 =N+ΔN
wherein:
Figure FDA00041223164300000213
Figure FDA00041223164300000214
Figure FDA00041223164300000215
Figure FDA0004122316430000031
solving the equation based on the concept of RCTLS can be achieved:
Figure FDA0004122316430000032
wherein:
Figure FDA0004122316430000033
and->
Figure FDA0004122316430000034
For the purpose of defining the intermediate variables,
step five: and solving regularization parameters contained in the solution obtained in the step 4 based on a criterion of minimizing the mean square error, and correcting the result obtained in the second step by using the solution obtained in the fourth step to obtain a final solution.
2. The regularization constraint weighted least squares based passive positioning method of claim 1, wherein: the positioning equation based on TDOA/FDOA obtained in the first step is as follows:
Figure FDA0004122316430000035
wherein: r is (r) i1 S is the measured distance difference between the primary station and the secondary station to the target i And
Figure FDA0004122316430000036
for receiving the position and velocity coordinates of the station, u o And->
Figure FDA0004122316430000037
Epsilon for the position and velocity coordinates of the object t =bΔr, error term of TDOA equation, +.>
Figure FDA0004122316430000038
Is the error term of the FDOA equation, wherein +.>
Figure FDA0004122316430000039
3. The regularization constraint weighted least squares based passive positioning method of claim 2, wherein: the third step is as follows: solving regularization parameters in the solution obtained in the second step, and expressing the mean square error of the estimation error in the first step of estimation as:
Figure FDA00041223164300000310
solving the above equation based on a criterion that minimizes the mean square error may result in regularization parameters of:
Figure FDA00041223164300000311
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