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CN110176953B - A Planar Frequency Controlled Array Beamforming Method Based on Generalized Eigenvalue Decomposition - Google Patents

A Planar Frequency Controlled Array Beamforming Method Based on Generalized Eigenvalue Decomposition Download PDF

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CN110176953B
CN110176953B CN201910450444.8A CN201910450444A CN110176953B CN 110176953 B CN110176953 B CN 110176953B CN 201910450444 A CN201910450444 A CN 201910450444A CN 110176953 B CN110176953 B CN 110176953B
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antenna
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CN110176953A (en
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陈慧
程婕
万珂妙
王文钦
廖轶
张顺生
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University of Electronic Science and Technology of China
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    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/02Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas
    • H04B7/04Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas
    • H04B7/06Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas at the transmitting station
    • H04B7/0613Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas at the transmitting station using simultaneous transmission
    • H04B7/0615Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas at the transmitting station using simultaneous transmission of weighted versions of same signal
    • H04B7/0617Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas at the transmitting station using simultaneous transmission of weighted versions of same signal for beam forming
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/02Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas
    • H04B7/04Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas
    • H04B7/06Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas at the transmitting station
    • H04B7/0613Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas at the transmitting station using simultaneous transmission
    • H04B7/0615Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas at the transmitting station using simultaneous transmission of weighted versions of same signal
    • H04B7/0619Diversity systems; Multi-antenna system, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas at the transmitting station using simultaneous transmission of weighted versions of same signal using feedback from receiving side
    • H04B7/0621Feedback content
    • H04B7/0634Antenna weights or vector/matrix coefficients

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Abstract

本发明提供了一种基于广义特征值分解的平面频控阵波束形成方法,其实现方法如下:根据天线的阵元个数、载波频率、相邻天线阵元间的频偏值和相邻天线阵元间的间距构建平面频控阵;根据所述平面频控阵构建其相应的远场发射波束图;利用能量聚集算法BCE分别对所述远场发射波束图的特征值和特征向量进行求解,得到远场发射波束图的最优权重矩阵,从而形成平面频控阵的波束。本发明利用广义特征值分解求解最优发射权重,可在期望区域内形成聚焦点波束,解决了线性频控阵无法形成良好点波束的问题。

Figure 201910450444

The present invention provides a plane frequency-controlled array beam forming method based on generalized eigenvalue decomposition, and the realization method is as follows: The distance between the array elements constructs a plane frequency-controlled array; constructs its corresponding far-field transmit beam pattern according to the plane frequency-controlled array; uses the energy gathering algorithm BCE to solve the eigenvalues and eigenvectors of the far-field transmit beam pattern respectively , the optimal weight matrix of the far-field transmit beam pattern is obtained, thereby forming the beam of the planar frequency-controlled array. The invention utilizes generalized eigenvalue decomposition to solve the optimal transmission weight, can form a focused spot beam in a desired area, and solves the problem that a linear frequency-controlled array cannot form a good spot beam.

Figure 201910450444

Description

一种基于广义特征值分解的平面频控阵波束形成方法A Planar Frequency Controlled Array Beamforming Method Based on Generalized Eigenvalue Decomposition

技术领域technical field

本发明属于频控阵雷达技术领域,尤其涉及一种基于广义特征值分解的平面频控阵波束形成方法。The invention belongs to the technical field of frequency-controlled array radar, and in particular relates to a plane frequency-controlled array beam forming method based on generalized eigenvalue decomposition.

背景技术Background technique

频控阵雷达因其特有的距离-角度依赖性而在雷达系统、无线通信、雷达成像、目标估计与追踪、干扰及抗干扰等领域有着非常广泛的应用。均匀线形频控阵虽然能够形成具有角度-距离依赖性的发射波束,但其波束图的距离和方位角耦合,在距离-角度二维平面内呈S形峰脊状,并非理想的单峰波束即点波束。为形成点波束,需要角度维和距离维解耦,而线形频控阵无法产生真正意义上的点波束,即使通过配置线型频控阵的参数,比如频偏、阵元间隔等,能够形成近似的点波束,但其代价是波束分辨率的损失。目前针对平面频控阵的波束形成方法可以采用蚁群算法优化频偏,但此方法计算过程相对复杂。Due to its unique range-angle dependence, frequency-controlled array radar has a very wide range of applications in radar systems, wireless communications, radar imaging, target estimation and tracking, jamming and anti-jamming. Although the uniform linear frequency-controlled array can form a transmission beam with angle-distance dependence, the distance and azimuth angle coupling of its beam pattern are S-shaped peaks and ridges in the distance-angle two-dimensional plane, which is not an ideal single-peak beam. That is spot beam. In order to form a spot beam, decoupling of the angle dimension and the distance dimension is required, and the linear frequency-controlled array cannot generate spot beams in the true sense. , but at the cost of a loss of beam resolution. At present, the beamforming method for planar frequency-controlled array can use ant colony algorithm to optimize the frequency offset, but the calculation process of this method is relatively complicated.

发明内容SUMMARY OF THE INVENTION

针对现有技术中的上述不足,本发明提出一种基于广义特征值分解的平面频控阵波束形成方法,利用广义特征值分解求解最优发射权重,可在期望区域内形成聚焦点波束,解决了线性频控阵无法形成良好点波束的问题。In view of the above deficiencies in the prior art, the present invention proposes a plane frequency-controlled array beamforming method based on generalized eigenvalue decomposition, which utilizes generalized eigenvalue decomposition to solve the optimal transmission weight, and can form a focused spot beam in a desired area, solving the problem of This solves the problem that linear frequency-controlled arrays cannot form good spot beams.

为了达到以上目的,本发明采用的技术方案为:In order to achieve the above purpose, the technical scheme adopted in the present invention is:

本方案提供一种基于广义特征值分解的平面频控阵波束形成方法,包括如下步骤:This solution provides a planar frequency-controlled array beamforming method based on generalized eigenvalue decomposition, including the following steps:

S1、根据天线的阵元个数、载波频率、相邻天线阵元间的频偏值和相邻天线阵元间的间距构建平面频控阵;S1. Construct a planar frequency-controlled array according to the number of array elements of the antenna, the carrier frequency, the frequency offset value between adjacent antenna array elements and the spacing between adjacent antenna array elements;

S2、根据所述平面频控阵构建其相应的远场发射波束图;S2, constructing its corresponding far-field transmit beam pattern according to the planar frequency-controlled array;

S3、利用能量聚集算法BCE分别对所述远场发射波束图的特征值和特征向量进行求解,得到远场发射波束图的最优权重矩阵,从而形成平面频控阵的波束。S3. Use the energy aggregation algorithm BCE to solve the eigenvalues and eigenvectors of the far-field transmit beam pattern respectively to obtain an optimal weight matrix of the far-field transmit beam pattern, thereby forming a plane frequency-controlled array beam.

再进一步地,所述步骤S1中所述天线为全向天线。Still further, the antenna in the step S1 is an omnidirectional antenna.

再进一步地,所述平面频控阵由M×N个天线阵元个数构成,第一个天线的载波频率f0为10GHz,其中,Still further, the planar frequency-controlled array is composed of M×N antenna array elements, and the carrier frequency f 0 of the first antenna is 10 GHz, wherein,

所述天线阵元的x方向按等间距dx分布M个天线阵元,且相邻天线阵元间的频偏值Δfx依次按线性递增;The x direction of the antenna array element is distributed with M antenna array elements at equal intervals d x , and the frequency offset value Δf x between adjacent antenna array elements is linearly increased in sequence;

所述天线阵元的y方向按等间距dy分布N个天线阵元,且相邻天线阵元间的频偏值Δfy依次按线性递增。In the y direction of the antenna array elements, N antenna array elements are distributed at equal intervals dy, and the frequency offset value Δf y between adjacent antenna array elements increases linearly in sequence.

再进一步地,所述x方向与y方向的相邻天线的频偏值均为30KHz。Still further, the frequency offset values of the adjacent antennas in the x-direction and the y-direction are both 30KHz.

再进一步地,所述x方向与y方向的相邻天线的间距均为0.03m。Still further, the distances between adjacent antennas in the x-direction and the y-direction are both 0.03m.

再进一步地,所述远场发射波束图

Figure BDA0002074970390000021
的表达式如下:Still further, the far-field transmit beam pattern
Figure BDA0002074970390000021
The expression is as follows:

Figure BDA0002074970390000022
Figure BDA0002074970390000022

Figure BDA0002074970390000023
Figure BDA0002074970390000023

Figure BDA0002074970390000024
and
Figure BDA0002074970390000024

其中,exp{·}表示以自然常数e为底的指数函数,j表示复数单位,f0表示发射信号的中心频率,t表示时间,r表示参考阵元到目标点的距离,c表示光速,W表示天线阵元的发射权重矩阵,M表示x方向的天线阵元个数,N表示y方向的天线阵元个数,m表示天线阵元沿x方向的序号,m=0,1,2,...M,n表示阵元沿y方向的序号,n=0,1,2,...N,W*表示发射矩阵W的共轭,⊙表示哈达玛积,A表示阵列因子,wM-1,N-1表示发射矩阵元素,aM-1,N-1表示阵列因子元素,amn表示第mn个阵元的阵列因子,Δfmn表示第mn个阵元的频偏值,dmn表示第mn个阵元的阵元间距,θ表示目标点的倒向角,

Figure BDA0002074970390000031
表示目标点的方位角。Among them, exp{·} represents the exponential function with the natural constant e as the base, j represents the complex unit, f 0 represents the center frequency of the transmitted signal, t represents the time, r represents the distance from the reference array element to the target point, c represents the speed of light, W represents the transmit weight matrix of the antenna elements, M represents the number of antenna elements in the x direction, N represents the number of antenna elements in the y direction, m represents the serial number of the antenna elements along the x direction, m=0,1,2 ,...M, n denotes the array element number along the y direction, n=0,1,2,...N, W * denotes the conjugate of the emission matrix W, ⊙ denotes the Hadamard product, A denotes the array factor, w M-1, N-1 represents the transmission matrix element, a M-1, N-1 represents the array factor element, a mn represents the array factor of the mn-th array element, Δf mn represents the frequency offset value of the mn-th array element , d mn represents the array element spacing of the mnth array element, θ represents the inversion angle of the target point,
Figure BDA0002074970390000031
Indicates the azimuth of the target point.

再进一步地,所述步骤S3中远场发射波束图的最优权重矩阵vec(Wopt)的表达式如下:Still further, the expression of the optimal weight matrix vec(W opt ) of the far-field transmit beam pattern in the step S3 is as follows:

Figure BDA0002074970390000032
Figure BDA0002074970390000032

其中,

Figure BDA0002074970390000033
表示求解最大权向量,vec(W)H表示发射权重的矩阵向量化的共轭转置,vec(W)表示发射权重矩阵向量化,A表示在期望辐射范围的功率,B表示总辐射范围内的功率。in,
Figure BDA0002074970390000033
Represents solving the maximum weight vector, vec(W) H represents the conjugate transpose of the matrix vectorization of the emission weight, vec(W) represents the vectorization of the transmission weight matrix, A represents the power in the desired radiation range, and B represents the total radiation range. of power.

本发明的有益效果:Beneficial effects of the present invention:

本发明根据天线的阵元个数、载波频率、相邻天线阵元间的频偏值和相邻天线阵元间的间距构建平面频控阵;根据所述平面频控阵构建其相应的远场发射波束图;利用能量聚集算法BCE分别对所述远场发射波束图的特征值和特征向量进行求解,得到远场发射波束图的最优权重矩阵,从而形成平面频控阵的波束,本发明通过以上步骤,利用广义特征值分解求解最优发射权重,可在期望区域内形成聚焦点波束,解决了线性频控阵无法形成良好点波束的问题The present invention constructs a plane frequency controlled array according to the number of antenna elements, the carrier frequency, the frequency offset value between adjacent antenna elements and the spacing between adjacent antenna elements; Field emission beam pattern; use the energy aggregation algorithm BCE to solve the eigenvalues and eigenvectors of the far-field emission beam pattern respectively, and obtain the optimal weight matrix of the far-field emission beam pattern, thereby forming the beam of the planar frequency-controlled array. Through the above steps, the invention uses generalized eigenvalue decomposition to solve the optimal transmission weight, which can form a focused spot beam in a desired area, and solves the problem that a linear frequency-controlled array cannot form a good spot beam.

附图说明Description of drawings

图1为本发明的方法流程图。FIG. 1 is a flow chart of the method of the present invention.

图2为本实施例中的平面频控阵模型示意图。FIG. 2 is a schematic diagram of a planar frequency controlled array model in this embodiment.

图3为本实施例中的平面频控阵三维空间发射模型图。FIG. 3 is a diagram of a three-dimensional space emission model of a planar frequency-controlled array in this embodiment.

图4为本实施例中未使用优化权重矩阵对应的平面频控阵归一化三维波束图。FIG. 4 does not use the normalized three-dimensional beam pattern of the planar frequency-controlled array corresponding to the optimized weight matrix in this embodiment.

图5为本实施例中未使用优化权重矩阵对应的平面频控阵归一化二维平面波束图。FIG. 5 is a normalized two-dimensional planar beam diagram corresponding to a planar frequency-controlled array without using an optimized weight matrix in this embodiment.

图6为本实施例中目标区域a的平面频控阵点波束图。FIG. 6 is a plane frequency-controlled array spot beam diagram of the target area a in this embodiment.

图7为本实施例中目标区域b的平面频控阵点波束图。FIG. 7 is a plane frequency-controlled array spot beam diagram of the target area b in this embodiment.

具体实施方式Detailed ways

下面对本发明的具体实施方式进行描述,以便于本技术领域的技术人员理解本发明,但应该清楚,本发明不限于具体实施方式的范围,对本技术领域的普通技术人员来讲,只要各种变化在所附的权利要求限定和确定的本发明的精神和范围内,这些变化是显而易见的,一切利用本发明构思的发明创造均在保护之列。The specific embodiments of the present invention are described below to facilitate those skilled in the art to understand the present invention, but it should be clear that the present invention is not limited to the scope of the specific embodiments. For those of ordinary skill in the art, as long as various changes Such changes are obvious within the spirit and scope of the present invention as defined and determined by the appended claims, and all inventions and creations utilizing the inventive concept are within the scope of protection.

实施例Example

如图1所示,本发明公开了一种基于广义特征值分解的平面频控阵波束形成方法,其实施方法如下:As shown in FIG. 1 , the present invention discloses a planar frequency-controlled array beamforming method based on generalized eigenvalue decomposition, and its implementation method is as follows:

S1、根据天线的阵元个数、天线阵元的载波频率、相邻天线阵元间的频偏值和相邻天线阵元间的间距构建平面频控阵,具体地,如图2-图3所示,由M×N个阵元构成一个平面频控阵,x方向阵元按dx等间距分布M个阵元,各阵元频偏依次按Δfx线性递增,y方向阵元按dy等间距分布N个阵元,各阵元频偏依次按Δfy线性递增,平面频控阵发射信号,远场处观测点的球面坐标为

Figure BDA0002074970390000041
其中,
Figure BDA0002074970390000042
是目标点的方位角,取值范围为[0,2π);θ是目标点的俯仰角,取值范围为[0,π);r为观测点到参考点的距离,取值范围为[Rmin,∞),其中,Rmin是使观测点满足远场假设的最小距离,本发明实例中,假定的平面频控阵模型中的天线均采用全向天线,在不考虑能量随距离衰减的情况下,设置全向天线阵元个数为M=N=10,第一个全向天线(参考阵元)的载波频率为f0=10GHz,相邻全向天线的频偏值为Δfx=Δfy=30KHz,相邻全向天线的间隔为dx=dy=0.03m,俯仰角θ=90°,即阵列所在平面;S1. Build a planar frequency-controlled array according to the number of antenna elements, the carrier frequency of the antenna elements, the frequency offset between adjacent antenna elements, and the spacing between adjacent antenna elements. Specifically, as shown in Figure 2-Figure As shown in 3, a planar frequency-controlled array is composed of M×N array elements. The array elements in the x direction are distributed with M array elements at equal intervals of d x , and the frequency offset of each array element increases linearly according to Δf x . N array elements are distributed at equal intervals in d y , and the frequency offset of each array element increases linearly by Δf y in turn. The plane frequency-controlled array transmits signals. The spherical coordinates of the observation point at the far field are
Figure BDA0002074970390000041
in,
Figure BDA0002074970390000042
is the azimuth angle of the target point, the value range is [0, 2π); θ is the pitch angle of the target point, the value range is [0, π); r is the distance from the observation point to the reference point, the value range is [ R min ,∞), where R min is the minimum distance for the observation point to satisfy the assumption of the far field. In the example of the present invention, the antennas in the assumed planar frequency controlled array model are omnidirectional antennas, and the attenuation of energy with distance is not considered. In the case of , set the number of omnidirectional antenna array elements to M=N=10, the carrier frequency of the first omnidirectional antenna (reference array element) is f 0 =10GHz, and the frequency offset value of adjacent omnidirectional antennas is Δf x = Δf y = 30KHz, the interval between adjacent omnidirectional antennas is d x = dy = 0.03m, and the elevation angle θ = 90°, that is, the plane where the array is located;

S2、根据所述平面频控阵构建其相应的远场发射波束图,在具体实施例中,假定位于坐标系原点所在位置的阵元为第一个全向天线(参考阵元),记为e00,则其他位置处的阵元可记为emn,其中,m表示天线阵元沿x方向的序号,m=0,1,2,...M,n表示阵元沿y方向的序号,n=0,1,2,...N,阵元emn的发射单频信号smn(t),如式(1)所示:S2. Construct its corresponding far-field transmit beam pattern according to the planar frequency-controlled array. In a specific embodiment, it is assumed that the array element located at the origin of the coordinate system is the first omnidirectional antenna (reference array element), denoted as e 00 , then the array elements at other positions can be recorded as e mn , where m represents the serial number of the antenna array element along the x direction, m=0, 1, 2,...M, n represents the array element along the y direction Serial number, n=0, 1, 2,...N, the single-frequency signal s mn (t) transmitted by the array element e mn , as shown in formula (1):

smn(t)=exp(j2πfmnt) (1)s mn (t)=exp(j2πf mn t) (1)

远场观测点

Figure BDA0002074970390000051
处接收到的信号
Figure BDA0002074970390000052
如式(2)所示:far-field observation point
Figure BDA0002074970390000051
signal received at
Figure BDA0002074970390000052
As shown in formula (2):

Figure BDA0002074970390000053
Figure BDA0002074970390000053

其中,exp{·}表示以自然常数e为底的指数函数,fmn表示第mn个阵元的工作频率,t表示时间,

Figure BDA0002074970390000054
表示第mn个阵元的权重共轭,rmn表示第mn个阵元的倾斜距离,W={wmn}M×N为天线阵元的发射权重矩阵,
Figure BDA0002074970390000055
为阵元emn的天线方向图,假定阵列天线的一致性较好,且每个阵元天线是各向同性点源,且频域响应在载频f0附近平坦,则有
Figure BDA0002074970390000056
exp{·}表示以自然常数e为底的指数函数,阵元emn的载频fmn=f0+mΔfx+nΔfy,m=0,1,2,...,M-1,n=0,1,2,...,N-1,f0为参考阵元e00的载频,远场观测点到阵元emn的距离
Figure BDA0002074970390000057
m=0,1,2,...,M-1,n=0,1,2,...,N-1,简化式(2)为:Among them, exp{·} represents the exponential function with the natural constant e as the base, f mn represents the operating frequency of the mn-th array element, t represents the time,
Figure BDA0002074970390000054
represents the weight conjugate of the mn-th array element, r mn represents the tilt distance of the mn-th array element, W={w mn } M×N is the transmit weight matrix of the antenna element,
Figure BDA0002074970390000055
is the antenna pattern of the array element e mn , assuming that the consistency of the array antennas is good, and each array element antenna is an isotropic point source, and the frequency domain response is flat near the carrier frequency f 0 , then there are
Figure BDA0002074970390000056
exp{·} represents the exponential function with the natural constant e as the base, the carrier frequency of the array element e mn f mn =f 0 +mΔf x +nΔf y , m=0,1,2,...,M-1, n=0,1,2,...,N-1, f 0 is the carrier frequency of the reference array element e 00 , the distance from the far-field observation point to the array element e mn
Figure BDA0002074970390000057
m=0,1,2,...,M-1,n=0,1,2,...,N-1, the simplified formula (2) is:

Figure BDA0002074970390000061
Figure BDA0002074970390000061

其中,Δfmn=mΔfx+nΔfy

Figure BDA0002074970390000062
Δfx表示x方向相邻天线阵元的频偏值,Δfy表示y方向相邻天线阵元的频偏值,Δfmn表示第mn个阵元的频偏值,dmn表示第mn个阵元的阵元间隔,θ表示目标点的倒向角,
Figure BDA0002074970390000063
表示目标点的方位角;where Δf mn =mΔf x +nΔf y ,
Figure BDA0002074970390000062
Δf x represents the frequency offset value of the adjacent antenna element in the x direction, Δf y represents the frequency offset value of the adjacent antenna element in the y direction, Δf mn represents the frequency offset value of the mnth array element, and dmn represents the mnth array element. element spacing, θ represents the reversal angle of the target point,
Figure BDA0002074970390000063
represents the azimuth of the target point;

假定相邻天线的频偏值Δfx和Δfy,相邻天线阵元间距dx和dy满足下列条件:Assuming the frequency offset values of adjacent antennas Δf x and Δf y , the distances d x and dy between adjacent antenna elements satisfy the following conditions:

Figure BDA0002074970390000064
Figure BDA0002074970390000064

则进一步简化式(4)为:Then formula (4) is further simplified as:

Figure BDA0002074970390000065
Figure BDA0002074970390000065

其中,AFx为x轴上的线形频控阵阵列因子,AFy为y轴上的线形频控阵阵列因子,分别可以表示为:Among them, AF x is the linear frequency-controlled array array factor on the x-axis, and AF y is the linear frequency-controlled array array factor on the y-axis, which can be expressed as:

Figure BDA0002074970390000066
Figure BDA0002074970390000066

Figure BDA0002074970390000067
Figure BDA0002074970390000067

其中,

Figure BDA0002074970390000068
表示x方向上的权值共轭,
Figure BDA0002074970390000069
表示y方向上的权值共轭,x轴上的频控阵权重wx={wxm}M×1和y轴上的频控阵权重wy={wyn}N×1表示为:in,
Figure BDA0002074970390000068
represents the weight conjugate in the x direction,
Figure BDA0002074970390000069
Represents the weight conjugate in the y-direction, the frequency-controlled array weight w x ={w xm } M×1 on the x-axis and the frequency-controlled array weight w y ={w yn } N×1 on the y-axis are expressed as:

W=wx Twy={wxm·wyn}M×N (8)W=w x T w y ={w xm ·w yn } M×N (8)

其中,wx T表示x方向上的权向量转置,wy表示y方向上的权向量,wxm表示x方向上的权值,wyn表示表示y方向上的权值,M×N表示一个平面频控阵模型,平面频控阵的发射权重矩阵分解为两个线阵频控阵发射权重向量,则平面频控阵的发射波束图可以写成如下矩阵形式:Among them, w x T represents the weight vector transposition in the x direction, w y represents the weight vector in the y direction, w xm represents the weight value in the x direction, w yn represents the weight value in the y direction, and M×N represents the weight vector in the y direction. For a planar frequency controlled array model, the transmit weight matrix of the planar frequency controlled array is decomposed into two linear array frequency controlled array transmit weight vectors, then the transmit beam pattern of the planar frequency controlled array can be written in the following matrix form:

Figure BDA0002074970390000071
Figure BDA0002074970390000071

其中:in:

Figure BDA0002074970390000072
Figure BDA0002074970390000072

Figure BDA0002074970390000073
and
Figure BDA0002074970390000073

其中,exp{·}表示以自然常数e为底的指数函数,j表示复数单位,f0表示发射信号的中心频率,t表示时间,r表示参考阵元到目标点的距离,c表示光速,W表示天线阵元的发射权重矩阵,M表示x方向的天线阵元个数,N表示y方向的天线阵元个数,m表示天线阵元沿x方向的序号,m=0,1,2,...M,n表示阵元沿y方向的序号,n=0,1,2,...N,W*表示发射矩阵W的共轭,⊙表示哈达玛积,A表示阵列因子,wM-1,N-1表示发射矩阵元素,aM-1,N-1表示阵列因子元素,amn表示第mn个阵元的阵列因子,Δfmn表示第mn个阵元的频偏值,dmn表示第mn个阵元的阵元间距,θ表示目标点的倒向角,

Figure BDA0002074970390000074
表示目标点的方位角;Among them, exp{·} represents the exponential function with the natural constant e as the base, j represents the complex unit, f 0 represents the center frequency of the transmitted signal, t represents the time, r represents the distance from the reference array element to the target point, c represents the speed of light, W represents the transmit weight matrix of the antenna elements, M represents the number of antenna elements in the x direction, N represents the number of antenna elements in the y direction, m represents the serial number of the antenna elements along the x direction, m=0,1,2 ,...M, n denotes the array element number along the y direction, n=0,1,2,...N, W * denotes the conjugate of the emission matrix W, ⊙ denotes the Hadamard product, A denotes the array factor, w M-1, N-1 represents the transmission matrix element, a M-1, N-1 represents the array factor element, a mn represents the array factor of the mn-th array element, Δf mn represents the frequency offset value of the mn-th array element , d mn represents the array element spacing of the mnth array element, θ represents the inversion angle of the target point,
Figure BDA0002074970390000074
represents the azimuth of the target point;

S3、利用能量聚集算法BCE分别对所述远场发射波束图的特征值和特征向量进行求解,得到远场发射波束图的最优权重矩阵,从而形成平面频控阵的波束,在具体实施例中,将远场发射波束图和能量聚集算法BCE相结合,提出基于广义特征值分解的平面频控阵点波束形成方法:S3, using the energy aggregation algorithm BCE to solve the eigenvalues and eigenvectors of the far-field transmit beam pattern respectively, to obtain the optimal weight matrix of the far-field transmit beam pattern, thereby forming the beam of the planar frequency-controlled array, in a specific embodiment In , a planar frequency-controlled array spot beamforming method based on generalized eigenvalue decomposition is proposed by combining the far-field transmit beam pattern with the energy gathering algorithm BCE:

在具体实施例中,平面频控阵的发射波束图

Figure BDA0002074970390000081
表示为:In a specific embodiment, the transmit beam pattern of the planar frequency controlled array
Figure BDA0002074970390000081
Expressed as:

Figure BDA0002074970390000082
Figure BDA0002074970390000082

进一步推导为:It is further derived as:

Figure BDA0002074970390000083
Figure BDA0002074970390000083

其中,A表示阵列因子,wx H表示x方向上的权向量的共轭转置,ax(·)表示x方向上的阵列因子,wy H表示y方向上的权向量的共轭转置,ay(·)表示y方向上的权向量,W表示发射权重矩阵,H表示求共轭转置,vec(·)表示将矩阵进行向量化处理;Among them, A represents the array factor, w x H represents the conjugate transpose of the weight vector in the x direction, a x ( ) represents the array factor in the x direction, and w y H represents the conjugate transpose of the weight vector in the y direction set, a y ( ) represents the weight vector in the y direction, W represents the emission weight matrix, H represents the conjugate transpose, and vec( ) represents the vectorization of the matrix;

定义能量聚集算法BCE为期望范围内的发射功率

Figure BDA0002074970390000084
与总发射功率PΩ的比值,其表达式为:Define the energy aggregation algorithm BCE as the transmit power within the desired range
Figure BDA0002074970390000084
The ratio to the total transmit power P Ω , its expression is:

Figure BDA0002074970390000085
Figure BDA0002074970390000085

其中,

Figure BDA0002074970390000086
Ω0和Ω分别表示期望的波束辐射范围和总的波束辐射范围,
Figure BDA0002074970390000087
表示期望辐射范围内的积分,∫Ω表示总辐射范围内的积分,d表示微分符号,θ表示目标点的倒向角,
Figure BDA0002074970390000088
表示目标点的方位角,r表示参考阵元到目标点的距离,则in,
Figure BDA0002074970390000086
Ω 0 and Ω denote the desired beam radiation range and the total beam radiation range, respectively,
Figure BDA0002074970390000087
represents the integral in the expected radiation range, ∫ Ω represents the integral in the total radiation range, d represents the differential sign, θ represents the reversal angle of the target point,
Figure BDA0002074970390000088
represents the azimuth of the target point, r represents the distance from the reference array element to the target point, then

Figure BDA0002074970390000091
Figure BDA0002074970390000091

其中,in,

Figure BDA0002074970390000092
Figure BDA0002074970390000092

Figure BDA0002074970390000093
Figure BDA0002074970390000093

Figure BDA0002074970390000094
上式中,
Figure BDA0002074970390000095
表示期望辐射范围内的三重积分,∫∫∫Ω表示总辐射范围内的三重积分,θ1和θ2均表示期望范围的倒向角范围边界,
Figure BDA0002074970390000096
Figure BDA0002074970390000097
均表示期望范围的方位角范围边界,对于距离维,由于其周期性,r取一个距离周期的范围内,针对任意发射孔径和目标区域波束形成问题,可以构造成广义特征值分解问题,对所述远场发射波束图的特征值和特征向量进行求解,得到关于最大能量聚集算法BCE的最优发射阵列权值的显式表达式:
Figure BDA0002074970390000094
In the above formula,
Figure BDA0002074970390000095
represents the triple integral over the desired radiation range, ∫∫∫ Ω denotes the triple integral over the total radiation range, both θ 1 and θ 2 represent the reversal angle range boundary of the desired range,
Figure BDA0002074970390000096
and
Figure BDA0002074970390000097
Both represent the azimuth range boundary of the desired range. For the range dimension, due to its periodicity, r is within the range of a range period. For the beamforming problem of any transmit aperture and target area, it can be constructed as a generalized eigenvalue decomposition problem. The eigenvalues and eigenvectors of the far-field transmit beam pattern are solved, and the explicit expression of the optimal transmit array weights for the maximum energy gathering algorithm BCE is obtained:

Figure BDA0002074970390000098
Figure BDA0002074970390000098

其中,

Figure BDA0002074970390000099
表示求解最大权向量,vec(W)H表示发射权重的矩阵向量化的共轭转置,vec(W)表示发射权重矩阵向量化,A表示在期望辐射范围的功率,B表示总辐射范围内的功率,若A和B是厄米特Hermitian矩阵且具有正定特性,则使最大能量聚集算法BCE最大的权向量vec(Wopt)与广义特征值问题的最大特征值对应的特征向量相等,确定A和B项后,通过计算式(14)中最大的特征值和对应的特征向量得到最优解vec(Wopt),将式(14)中的结果带入代入式(13),最终得到期望范围内的发射功率与总发射功率的比值:in,
Figure BDA0002074970390000099
Represents solving the maximum weight vector, vec(W) H represents the conjugate transpose of the matrix vectorization of the emission weight, vec(W) represents the vectorization of the transmission weight matrix, A represents the power in the desired radiation range, and B represents the total radiation range. If A and B are Hermitian matrices and have positive definite characteristics, then make the maximum weight vector vec(W opt ) of the maximum energy aggregation algorithm BCE equal to the eigenvector corresponding to the maximum eigenvalue of the generalized eigenvalue problem, determine After A and B terms, the optimal solution vec(W opt ) is obtained by calculating the largest eigenvalue and corresponding eigenvector in equation (14), and the result in equation (14) is substituted into equation (13), and finally we get Ratio of transmit power in desired range to total transmit power:

Figure BDA00020749703900000910
Figure BDA00020749703900000910

本实施例中,如图6与图7所示,根据基于广义特征值分解的结果获得针对目标区域aΩ1:[70°,90°],[29km,32km]和目标区域bΩ2:[30°,50°],[39km,42km]相应的10×10权矩阵元素分别为0.5274、0.5972、0.8933、0.9558、0.9966、0.9966、0.9558、0.8933、0.5972、0.5274(仅给出对角元素)...和0.2826、0.4692、0.7590、0.9193、0.9893、0.9893、0.9193、0.7590、0.4692、0.2826(仅给出对角元素)...,相应的平面频控阵在两个目标区域处形成的二维发射点波束图,其中,Ω1表示目标区域a,Ω2表示目标区域b,当发射权重矩阵为全1矩阵时、即未使用优化权重矩阵,相应的平面频控阵的归一化三维波束图如图4所示,二维平面图如图5所示,图4表示平面频控阵在未采用能量聚集波束形成算法下的归一化三维波束图,图5表示所对应的二维波束图,通过与图6,7(图6和图7是采用了能量聚集波束形成算法)对比可以看出本次采用的能量聚集波束形成算法可以通过设定所需的聚焦范围来控制其点波束的聚焦位置。In this embodiment, as shown in FIG. 6 and FIG. 7 , according to the results based on generalized eigenvalue decomposition, the target area aΩ 1 : [70°, 90°], [29km, 32km] and the target area bΩ 2 : [30 °, 50°], [39km, 42km] The corresponding 10×10 weight matrix elements are 0.5274, 0.5972, 0.8933, 0.9558, 0.9966, 0.9966, 0.9558, 0.8933, 0.5972, 0.5274 (only the diagonal elements are given).. .and 0.2826, 0.4692, 0.7590, 0.9193, 0.9893, 0.9893, 0.9193, 0.7590, 0.4692, 0.2826 (only diagonal elements are given)..., the corresponding two-dimensional emissions formed by the planar frequency control array at the two target areas Spot beam pattern, where Ω 1 represents the target area a, Ω 2 represents the target area b, when the transmit weight matrix is an all-one matrix, that is, the optimized weight matrix is not used, the corresponding normalized three-dimensional beam pattern of the planar frequency control array As shown in Figure 4, the two-dimensional plane diagram is shown in Figure 5. Figure 4 shows the normalized three-dimensional beam diagram of the plane frequency controlled array without using the energy-focusing beamforming algorithm, and Figure 5 shows the corresponding two-dimensional beam diagram. By comparing with Figures 6 and 7 (Figures 6 and 7 use the energy-focusing beamforming algorithm), it can be seen that the energy-focusing beamforming algorithm adopted this time can control the focusing of its spot beam by setting the required focusing range Location.

Claims (6)

1.一种基于广义特征值分解的平面频控阵波束形成方法,其特征在于,包括如下步骤:1. a plane frequency-controlled array beamforming method based on generalized eigenvalue decomposition, is characterized in that, comprises the steps: S1、根据天线的阵元个数、载波频率、相邻天线阵元间的频偏值和相邻天线阵元间的间距构建平面频控阵;S1. Construct a planar frequency-controlled array according to the number of array elements of the antenna, the carrier frequency, the frequency offset value between adjacent antenna array elements and the spacing between adjacent antenna array elements; S2、根据所述平面频控阵构建其相应的远场发射波束图;S2, constructing its corresponding far-field transmit beam pattern according to the planar frequency-controlled array; S3、利用能量聚集算法BCE分别对所述远场发射波束图的特征值和特征向量进行求解,得到远场发射波束图的最优权重矩阵,从而形成平面频控阵的波束;S3, using the energy aggregation algorithm BCE to solve the eigenvalues and eigenvectors of the far-field transmit beam pattern respectively, to obtain the optimal weight matrix of the far-field transmit beam pattern, thereby forming the beam of the planar frequency-controlled array; 所述步骤S3中能量聚集算法BCE的表达式为:The expression of the energy aggregation algorithm BCE in the step S3 is:
Figure FDA0002497872190000011
Figure FDA0002497872190000011
其中,BCEopt表示能量聚焦算法BCE,vec(Wopt)H表示远场发射波束图的最优权重矩阵vec(Wopt)的共轭转置,A表示在期望辐射范围的功率,B表示总辐射范围内的功率;where BCE opt represents the energy focusing algorithm BCE, vec(W opt ) H represents the conjugate transpose of the optimal weight matrix vec(W opt ) of the far-field transmit beam pattern, A represents the power in the desired radiation range, and B represents the total power in the radiation range; 所述步骤S3中远场发射波束图的最优权重矩阵vec(Wopt)的表达式如下:The expression of the optimal weight matrix vec(W opt ) of the far-field transmit beam pattern in the step S3 is as follows:
Figure FDA0002497872190000012
Figure FDA0002497872190000012
其中,
Figure FDA0002497872190000013
表示求解最大权向量,vec(W)H表示发射权重的矩阵向量化的共轭转置,vec(W)表示发射权重矩阵向量化。
in,
Figure FDA0002497872190000013
Represents solving the maximum weight vector, vec(W) H represents the conjugate transpose of the matrix vectorization of the transmit weights, and vec(W) represents the vectorization of the transmit weight matrix.
2.根据权利要求1所述的基于广义特征值分解的平面频控阵波束形成方法,其特征在于,所述步骤S1中所述天线为全向天线。2 . The planar frequency-controlled array beamforming method based on generalized eigenvalue decomposition according to claim 1 , wherein the antenna in the step S1 is an omnidirectional antenna. 3 . 3.根据权利要求1所述的基于广义特征值分解的平面频控阵波束形成方法,其特征在于,所述平面频控阵由M×N个天线阵元个数构成,第一个天线的载波频率f0为10GHz,其中,M表示x方向的天线阵元个数,N表示y方向的天线阵元个数;3. The planar frequency-controlled array beamforming method based on generalized eigenvalue decomposition according to claim 1, wherein the planar frequency-controlled array is composed of M×N number of antenna array elements, and the first antenna The carrier frequency f 0 is 10GHz, where M represents the number of antenna elements in the x direction, and N represents the number of antenna elements in the y direction; 所述天线阵元的x方向按等间距dx分布M个天线阵元,且相邻天线阵元间的频偏值Δfx依次按线性递增;The x direction of the antenna array element is distributed with M antenna array elements at equal intervals d x , and the frequency offset value Δf x between adjacent antenna array elements is linearly increased in sequence; 所述天线阵元的y方向按等间距dy分布N个天线阵元,且相邻天线阵元间的频偏值Δfy依次按线性递增。In the y direction of the antenna array elements, N antenna array elements are distributed at equal intervals dy, and the frequency offset value Δf y between adjacent antenna array elements increases linearly in sequence. 4.根据权利要求3所述的基于广义特征值分解的平面频控阵波束形成方法,其特征在于,所述x方向与y方向的相邻天线的频偏值均为30KHz。4 . The planar frequency-controlled array beamforming method based on generalized eigenvalue decomposition according to claim 3 , wherein the frequency offset values of the adjacent antennas in the x-direction and the y-direction are both 30KHz. 5 . 5.根据权利要求3所述的基于广义特征值分解的平面频控阵波束形成方法,其特征在于,所述x方向与y方向的相邻天线的间距均为0.03m。5 . The planar frequency-controlled array beamforming method based on generalized eigenvalue decomposition according to claim 3 , wherein the distances between adjacent antennas in the x-direction and the y-direction are both 0.03m. 6 . 6.根据权利要求1所述的基于广义特征值分解的平面频控阵波束形成方法,其特征在于,所述远场发射波束图
Figure FDA0002497872190000021
的表达式如下:
6. The planar frequency-controlled array beamforming method based on generalized eigenvalue decomposition according to claim 1, wherein the far-field transmit beam pattern
Figure FDA0002497872190000021
The expression is as follows:
Figure FDA0002497872190000022
Figure FDA0002497872190000022
Figure FDA0002497872190000023
Figure FDA0002497872190000023
Figure FDA0002497872190000024
and
Figure FDA0002497872190000024
其中,exp{·}表示以自然常数e为底的指数函数,j表示复数单位,f0表示发射信号的中心频率,t表示时间,r表示参考阵元到目标点的距离,c表示光速,W表示天线阵元的发射权重矩阵,M表示x方向的天线阵元个数,N表示y方向的天线阵元个数,m表示天线阵元沿x方向的序号,m=0,1,2,...M-1,n表示阵元沿y方向的序号,n=0,1,2,...N-1,W*表示发射矩阵W的共轭,⊙表示哈达玛积,Y表示阵列因子,wM-1,N-1表示发射权重矩阵中的元素,aM-1,N-1表示阵列因子元素,amn表示第mn个阵元的阵列因子,θ表示目标点的倒向角,
Figure FDA0002497872190000031
表示目标点的方位角,Δfx表示沿x方向相邻天线阵元间的频偏值,Δfy表示沿y方向相邻天线阵元间的频偏值;dx表示沿x方向相邻天线阵元间的间距,dy表示沿y方向相邻天线阵元间的间距。
Among them, exp{·} represents the exponential function with the natural constant e as the base, j represents the complex unit, f 0 represents the center frequency of the transmitted signal, t represents the time, r represents the distance from the reference array element to the target point, c represents the speed of light, W represents the transmit weight matrix of the antenna elements, M represents the number of antenna elements in the x direction, N represents the number of antenna elements in the y direction, m represents the serial number of the antenna elements along the x direction, m=0,1,2 ,...M-1, n represents the serial number of the array element along the y direction, n=0,1,2,...N-1, W * represents the conjugate of the emission matrix W, ⊙ represents the Hadamard product, Y represents the array factor, w M-1, N-1 represents the element in the emission weight matrix, a M-1, N-1 represents the array factor element, a mn represents the array factor of the mnth array element, θ represents the target point inverted angle,
Figure FDA0002497872190000031
Represents the azimuth of the target point, Δf x represents the frequency offset between adjacent antenna elements along the x direction, Δf y represents the frequency offset between adjacent antenna elements along the y direction; d x represents the adjacent antenna along the x direction The spacing between array elements, dy represents the spacing between adjacent antenna array elements along the y direction.
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