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CN108196269B - Detection method of weak harmonic interference signal in satellite navigation anti-jamming antenna system - Google Patents

Detection method of weak harmonic interference signal in satellite navigation anti-jamming antenna system Download PDF

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CN108196269B
CN108196269B CN201711467672.3A CN201711467672A CN108196269B CN 108196269 B CN108196269 B CN 108196269B CN 201711467672 A CN201711467672 A CN 201711467672A CN 108196269 B CN108196269 B CN 108196269B
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王晓宇
张铁峰
张骅
董正芳
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
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    • G01S19/21Interference related issues ; Issues related to cross-correlation, spoofing or other methods of denial of service
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
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Abstract

The invention provides a method for detecting weak harmonic interference signals in a satellite navigation anti-interference antenna system, which adopts coherent accumulation of frequency spectrum energy as a check quantity and adaptively calculates a decision threshold to detect the weak harmonic interference signals in the satellite navigation anti-interference antenna system. Compared with a manual detection and identification method, the method has the characteristics that the detection threshold is determined in a self-adaptive mode on the basis of the sampling data by carrying out automatic detection processing on the original digital signals sampled by each channel in the system, and the detection probability of weak harmonic signals in the system can be effectively improved.

Description

卫星导航抗干扰天线系统内部弱谐波干扰信号检测方法Detection method of weak harmonic interference signal in satellite navigation anti-jamming antenna system

技术领域technical field

本发明属于卫星导航抗干扰领域,是一种对卫星导航抗干扰天线系统内部弱谐波干扰信号的检测方法。The invention belongs to the field of satellite navigation anti-jamming, and relates to a method for detecting weak harmonic interference signals inside a satellite navigation anti-jamming antenna system.

背景技术Background technique

目前,卫星导航抗干扰天线系统是保护卫星导航接收机在复杂电磁环境中正常工作的关键设备。为了使卫星导航抗干扰天线系统性能达到设计的最优值,需要在系统设计、生产以及调试过程中准确检测出系统内部影响系统性能的因素并消除。At present, the satellite navigation anti-jamming antenna system is the key equipment to protect the satellite navigation receiver to work normally in the complex electromagnetic environment. In order to make the performance of the satellite navigation anti-jamming antenna system reach the optimal value of the design, it is necessary to accurately detect and eliminate the factors that affect the system performance in the system design, production and debugging process.

卫星导航抗干扰天线系统主要由接收阵列天线、低噪声放大器、多通道射频组件以及数字信号处理组件等四部分组成。由于加工工艺、模拟元器件的工作特性等原因使得卫星导航抗干扰天线系统内部各通道中存在不同程度的弱谐波干扰信号。卫星导航抗干扰算法将系统内部的弱谐波干扰信号等效为从某一方向或多个方向入射的外界干扰信号进行抑制处理,因此将消耗抗干扰算法的部分处理自由度,影响抗干扰算法最多可抗干扰数目以及最大干扰抑制能力。The satellite navigation anti-jamming antenna system is mainly composed of four parts: receiving array antenna, low noise amplifier, multi-channel radio frequency components and digital signal processing components. Due to the processing technology and the working characteristics of the analog components, there are different degrees of weak harmonic interference signals in each channel of the satellite navigation anti-jamming antenna system. The satellite navigation anti-jamming algorithm suppresses the weak harmonic interference signal inside the system as the external interference signal incident from a certain direction or multiple directions, so it will consume part of the processing freedom of the anti-jamming algorithm and affect the anti-jamming algorithm. Maximum number of anti-interference and maximum interference suppression capability.

目前,对卫星导航抗干扰天线系统内部弱谐波干扰的检测主要是在调试过程中通过使用频谱分析仪等仪表工具对低噪声放大器、多通道射频组件等每个模块的输出信号进行观测分析。工程人员使用频谱分析仪的实时观测或最大保持功能对每个模块输出信号的频谱进行人工观测,检测识别系统内部的弱谐波干扰信号。对于功率接近或弱于系统噪声的弱谐波干扰信号,人工检测识别很容易造成漏检。At present, the detection of weak harmonic interference inside the satellite navigation anti-jamming antenna system is mainly to observe and analyze the output signals of each module such as low-noise amplifiers and multi-channel RF components by using instrumentation tools such as spectrum analyzers during the debugging process. Engineers use the real-time observation or maximum hold function of the spectrum analyzer to manually observe the spectrum of the output signal of each module to detect and identify weak harmonic interference signals within the system. For weak harmonic interference signals whose power is close to or weaker than system noise, manual detection and identification can easily lead to missed detection.

发明内容SUMMARY OF THE INVENTION

为了克服现有技术的不足,本发明提供一种卫星导航抗干扰天线系统内部弱谐波干扰信号检测方法,采用频谱能量相干累积作为检验量,并自适应计算判决门限对卫星导航抗干扰天线系统内部弱谐波干扰信号进行检测,可以有效提升对系统内部弱谐波信号的检测概率。In order to overcome the deficiencies of the prior art, the present invention provides a method for detecting weak harmonic interference signals inside a satellite navigation anti-jamming antenna system, which adopts the coherent accumulation of spectrum energy as a test quantity, and adaptively calculates a judgment threshold for the satellite navigation anti-jamming antenna system. The detection of internal weak harmonic interference signals can effectively improve the detection probability of weak harmonic signals in the system.

本发明解决其技术问题所采用的技术方案包括以下步骤:The technical scheme adopted by the present invention to solve its technical problem comprises the following steps:

第一步,在无外界电磁干扰的情况下,采集并存储设定时长T毫秒的卫星导航抗干扰天线的模数转换器输出的数字信号,对应的每个通道存储数据点数L=T×Fs×103,其中,Fs为模数转换器采样频率;The first step is to collect and store the digital signal output by the analog-to-digital converter of the satellite navigation anti-jamming antenna with a set duration of T milliseconds in the absence of external electromagnetic interference, and the corresponding number of data points stored in each channel L=T×F s ×10 3 , where F s is the sampling frequency of the analog-to-digital converter;

假设卫星导航抗干扰天线系统包含M个通道,则采集并存储的数据形成维数为L×M的矩阵,矩阵的第i列数据记为x(i)=[x0,x1,…,xL-1]TAssuming that the satellite navigation anti-jamming antenna system includes M channels, the collected and stored data forms a matrix with a dimension of L×M, and the data in the i-th column of the matrix is denoted as x(i)=[x 0 , x 1 ,..., x L-1 ] T ;

第二步,将数据向量x(i)划分为相互重叠的子数据段,每个子数据块的长度为N,N的取值设置为2的正整数次方,相邻两个子数据块之间的重叠率设置为50%,子数据块的总数

Figure BDA0001531420210000021
第k(k=1,2,…K)个子数据块记为xk(i);The second step is to divide the data vector x(i) into overlapping sub-data segments. The length of each sub-data block is N, and the value of N is set to a positive integer power of 2. Between two adjacent sub-data blocks The overlap ratio is set to 50%, the total number of sub-blocks
Figure BDA0001531420210000021
The kth (k=1,2,...K) sub-data block is denoted as x k (i);

第三步,构造一个大小为N×1维的向量y,将y中的每个元素初始化为0,表示为y0=0;The third step is to construct a vector y with a size of N×1 dimension, and initialize each element in y to 0, which is represented as y 0 =0;

第四步,依次对子数据块xk做快速傅里叶变换,设置快速傅里叶变换点数设置为N,快速傅里叶变换的结果记为Xk,Xk为N×1维的向量;计算Xk向量中第n个元素Xk(n)的模值的平方并累加在向量y中第n个元素中,yk(n)=yk-1(n)+|Xk(n)|2,n=1,2,...,N;The fourth step is to perform fast Fourier transform on the sub-data block x k in turn, set the number of fast Fourier transform points to N, the result of the fast Fourier transform is recorded as X k , and X k is an N×1-dimensional vector ; Calculate the square of the modulus value of the n-th element X k (n) in the X k vector and accumulate it in the n-th element in the vector y, y k (n)=y k-1 (n)+|X k ( n)| 2 , n=1,2,...,N;

第五步,根据卫星导航系统有效工作带宽B将向量y划分为S个子带,

Figure BDA0001531420210000022
Fs为采样频率,用ys表示向量y的第s个子带数据块,s=1,2,…,S;The fifth step is to divide the vector y into S sub-bands according to the effective working bandwidth B of the satellite navigation system,
Figure BDA0001531420210000022
F s is the sampling frequency, and y s represents the s-th subband data block of the vector y, s=1,2,...,S;

第六步,依次搜索子带数据块ys中的最大值ds,将S个子带中的最大值组成大小为S×1的向量d=[d1,d2,…,dS]TThe sixth step is to search for the maximum value d s in the sub-band data block y s in turn, and form the maximum value in the S sub-bands into a vector d=[d 1 ,d 2 ,...,d S ] T with a size of S×1 ;

第七步,搜索向量d中的最小值dmin,设噪声平均功率值Pnoise并初始化为0,设计数器J并初始化为0;依次判断向量y的每一个元素y(n)是否小于dmin,若小于dmin,则将y(n)在Pnoise中累加,计数器J计数加1,所有N个元素判断完成后,计算Pnoise/J并作为Pnoise更新值;The seventh step is to search for the minimum value d min in the vector d, set the average noise power value P noise and initialize it to 0, set the counter J and initialize it to 0; judge in turn whether each element y(n) of the vector y is less than d min , if it is less than d min , then y(n) is accumulated in P noise , the counter J counts up by 1, and after all N elements are judged, P noise /J is calculated and used as the updated value of P noise ;

第八步,以Pnoise的两倍作为判决门限值yt进行弱谐波干扰检测,依次判断向量y的每一个元素y(n)是否大于yt,若y(n)>yt,则判决为在频点

Figure BDA0001531420210000023
上存在干扰,并将f(n)输出。The eighth step is to use twice the P noise as the decision threshold y t to perform weak harmonic interference detection, and sequentially determine whether each element y(n) of the vector y is greater than y t , if y(n)>y t , Then it is judged that the frequency
Figure BDA0001531420210000023
There is interference on and f(n) is output.

本发明的有益效果是:通过多个数据块频谱能力的相干累积,使得卫星导航抗干扰天线系统内部弱谐波干扰信号的能量得到相干累积增益,提高了弱谐波干扰信号相对于系统热噪声的信噪比。同时,相对于固定判决门限,基于采样数据自适应计算判决门限可以进一步提升不同抗干扰天线系统状态差异情况下对弱谐波干扰的检测概率。本发明适用于对卫星导航抗干扰天线系统前期的最佳性能调试以及系统状态自检报告等。The beneficial effects of the present invention are: through the coherent accumulation of the spectral capabilities of a plurality of data blocks, the energy of the weak harmonic interference signal inside the satellite navigation anti-jamming antenna system can obtain a coherent accumulation gain, and the weak harmonic interference signal relative to the system thermal noise is improved. signal-to-noise ratio. At the same time, compared with the fixed decision threshold, the adaptive calculation of the decision threshold based on the sampled data can further improve the detection probability of weak harmonic interference in the case of different states of the anti-jamming antenna systems. The invention is suitable for the best performance debugging of the satellite navigation anti-jamming antenna system in the early stage, the system state self-check report, and the like.

附图说明Description of drawings

图1是本发明的方法流程图;Fig. 1 is the method flow chart of the present invention;

图2是相互重叠子数据块划分示意图。FIG. 2 is a schematic diagram of division of overlapping sub-data blocks.

具体实施方式Detailed ways

下面结合附图和实施例对本发明进一步说明,本发明包括但不仅限于下述实施例。The present invention will be further described below with reference to the accompanying drawings and embodiments, and the present invention includes but is not limited to the following embodiments.

本发明方法实现步骤如下:The implementation steps of the method of the present invention are as follows:

第一步:在无外界电磁干扰的情况下,采集并存储时长为T毫秒(T≥1)的卫星导航抗干扰天线模数转换器(A/D)输出的数字信号,对应的每个通道存储数据点数为L,L与存储时间长度T(量纲为毫秒,记为ms)以及模数转换器(A/D)采样频率Fs(量纲为兆赫兹,记为MHz)之间的计算关系为:The first step: in the absence of external electromagnetic interference, collect and store the digital signal output by the satellite navigation anti-jamming antenna analog-to-digital converter (A/D) with a duration of T milliseconds (T ≥ 1). The number of stored data points is L, the difference between L and the storage time length T (dimension is milliseconds, denoted as ms) and the sampling frequency of the analog-to-digital converter (A/D) F s (dimension is megahertz, denoted as MHz) The calculation relationship is:

L=T×Fs×103 (1)L=T×F s ×10 3 (1)

假设卫星导航抗干扰天线系统包含M个通道,则采集并存储的数据形成维数为L×M的矩阵。数据矩阵的第i(i=1,2,…,M)列数据记为x(i)=[x0,x1,…,xL-1]T,上标T为转置运算符。Assuming that the satellite navigation anti-jamming antenna system includes M channels, the collected and stored data form a matrix with a dimension of L×M. The i-th (i=1,2,...,M) column data of the data matrix is denoted as x(i)=[x 0 ,x 1 ,...,x L-1 ] T , and the superscript T is the transpose operator.

第二步:将数据向量x(i)(i=1,2,…,M)划分为相互重叠的子数据段,设置每个子数据块的长度为N(N的取值设置为2的正整数次方,通常设置为1024或2048),相邻两个子数据块之间的重叠率设置为50%,子数据块的总数为K。在50%数据重叠率的条件下,K与N以及L之间的关系为;Step 2: Divide the data vector x(i) (i=1,2,...,M) into overlapping sub-data segments, and set the length of each sub-data block to N (the value of N is set to a positive value of 2 Integer power, usually set to 1024 or 2048), the overlap rate between two adjacent sub-data blocks is set to 50%, and the total number of sub-data blocks is K. Under the condition of 50% data overlap rate, the relationship between K and N and L is;

Figure BDA0001531420210000031
Figure BDA0001531420210000031

其中,

Figure BDA0001531420210000032
为向下取整运算符。第k(k=1,2,…K)个子数据块记为xk(i)。in,
Figure BDA0001531420210000032
is the round-down operator. The kth (k=1, 2, . . . K ) sub-data block is denoted as x k (i).

第三步:构造一个大小为N×1维的向量,记为y,将y中的每个元素初始化为0,表示为:Step 3: Construct a vector of size N × 1, denoted as y, and initialize each element in y to 0, which is expressed as:

y0=0 (3)y 0 =0 (3)

其中,下标0表示初始状态,等式右侧的0表示包含有N个0元素的列向量。Among them, the subscript 0 represents the initial state, and the 0 on the right side of the equation represents a column vector containing N 0 elements.

第四步:依次对子数据块xk(k=1,2,…K)做快速傅里叶(FFT)变换,设置快速傅里叶变换点数设置为N,快速傅里叶变换的结果记为Xk,Xk为N×1维的向量。计算Xk向量中第n(n=1,2,...,N)个元素Xk(n)的模值的平方并累加在向量y中第n个元素中,计算表达式为:Step 4: Perform fast Fourier (FFT) transformation on the sub-data blocks x k (k=1,2,...K) in turn, set the number of fast Fourier transform points to N, and record the result of the fast Fourier transform. is X k , and X k is an N×1-dimensional vector. Calculate the square of the modulus value of the nth (n=1,2,...,N) element X k (n) in the X k vector and accumulate it in the nth element in the vector y. The calculation expression is:

yk(n)=yk-1(n)+|Xk(n)|2 (4)y k (n)=y k-1 (n)+|X k (n)| 2 (4)

第五步:根据卫星导航系统有效工作带宽B(量纲为兆赫兹)将向量y划分为S个子带,划分子带个数S与有效工作带宽B以及采样频率Fs之间的计算关系如下:Step 5: According to the effective working bandwidth B of the satellite navigation system (dimension is megahertz), the vector y is divided into S sub-bands, and the calculation relationship between the number of sub-bands S, the effective working bandwidth B and the sampling frequency F s is as follows :

Figure BDA0001531420210000041
Figure BDA0001531420210000041

其中,

Figure BDA0001531420210000042
为向下取整运算符。用ys(s=1,2,…,S)表示向量y的第s个子带数据块。in,
Figure BDA0001531420210000042
is the round-down operator. Let y s (s=1,2,...,S) denote the sth subband data block of the vector y.

第六步:依次搜索子带数据块ys(s=1,2,…,S)中的最大值ds,搜索算法采用“冒泡”排序法,将S个子带中的最大值组成大小为S×1的向量d:Step 6: Search for the maximum value d s in the sub-band data blocks y s (s=1,2,...,S) in turn. The search algorithm adopts the "bubble" sorting method, and the maximum value in the S sub-bands is composed of a size is a vector d of S × 1:

d=[d1,d2,…,dS]T (6)d=[d 1 ,d 2 ,...,d S ] T (6)

第七步:采用“冒泡”排序法搜索向量d中的最小值dmin,设噪声平均功率值Pnoise并初始化为0,设计数器J并初始化为0。依次判断向量y的每一个元素y(n)(n=1,2,...,N)是否小于dmin,若小于dmin,则将y(n)在Pnoise中累加,计数器J计数加1,所有N个元素判断完成后,计算Pnoise/J并作为Pnoise更新值。The seventh step: use the "bubble" sorting method to search for the minimum value d min in the vector d, set the average noise power value P noise and initialize it to 0, and set the counter J and initialize it to 0. Judging in turn whether each element y(n) (n=1,2,...,N) of the vector y is less than d min , if it is less than d min , y(n) is accumulated in P noise , and the counter J counts Add 1, after all N elements are judged, calculate P noise /J and use it as the updated value of P noise .

第八步:以Pnoise的两倍作为判决门限值yt进行弱谐波干扰检测,依次判断向量y的每一个元素y(n)(n=1,2,...,N)是否大于yt,若y(n)>yt,则判决为在频点f(n)上存在干扰,并将f(n)输出,f(n)计算如下:Step 8: Use twice the P noise as the judgment threshold y t to detect weak harmonic interference, and then judge whether each element y(n) (n=1,2,...,N) of the vector y is in turn. greater than y t , if y(n)>y t , it is judged that there is interference on the frequency point f(n), and f(n) is output, and f(n) is calculated as follows:

Figure BDA0001531420210000043
Figure BDA0001531420210000043

本发明适用于GPS、BDS和GLONASS等卫星导航抗干扰天线系统内部弱谐波干扰信号进行检测。以4单元BD2-B3频点抗干扰天线系统内部弱谐波干扰信号的检测为例阐述本发明的具体实施方式。The invention is suitable for detecting weak harmonic interference signals in satellite navigation anti-jamming antenna systems such as GPS, BDS and GLONASS. The specific embodiment of the present invention is described by taking the detection of weak harmonic interference signals in the 4-unit BD2-B3 frequency point anti-jamming antenna system as an example.

步骤1:在无外界电磁干扰的情况下,通过卫星导航抗干扰天线系统的数字信号处理模采集并存储所有4个通道的接收信号,采样频率Fs设置为62MHz,采样时长为2.1141ms,根据式(1)可以计算出每个通道采集并存储的信号点数L为131072。最终,4个通道存储的数据形成维数为131072×4的矩阵。Step 1: In the absence of external electromagnetic interference, the digital signal processing mode of the satellite navigation anti-jamming antenna system is used to collect and store the received signals of all 4 channels. The sampling frequency F s is set to 62MHz, and the sampling duration is 2.1141ms. According to Equation (1) can calculate that the number of signal points L collected and stored by each channel is 131072. Finally, the data stored in the 4 channels forms a matrix of dimension 131072×4.

步骤2:将数据矩阵的第i(i=1,2,…,4)列向量x(i)划分为相互重叠的子数据块,设置每个子数据块的长度为N为2048,相邻两个子数据块之间的重叠率设置为50%,则根据式(2)可计算出子数据块的总数为K为127。第k(k=1,2,…127)个子数据块记为xk(i)。图2所示为相互重叠的子数据块划分过程示意图。Step 2: Divide the i-th (i=1,2,...,4) column vector x(i) of the data matrix into overlapping sub-data blocks, set the length of each sub-data block to N is 2048, and the adjacent two The overlap rate between the sub-data blocks is set to 50%, then according to formula (2), the total number of sub-data blocks can be calculated as K is 127. The kth (k=1, 2, . . . 127) sub-data block is denoted as x k (i). FIG. 2 is a schematic diagram showing the division process of overlapping sub-data blocks.

步骤3:构造一个大小为2048×1维的向量,记为y,将y中的每个元素初始化为0。Step 3: Construct a vector of size 2048×1 dimension, denoted as y, and initialize each element in y to 0.

步骤4:依次对子数据块xk(i)(k=1,2,…127)做快速傅里叶(FFT)变换,设置快速傅里叶变换点数设置为2048,快速傅里叶变换的结果记为Xk,Xk为2048×1维的向量。按照式(5)计算Xk向量中第n(n=1,2,...,2048)个元素Xk(n)的模值的平方并累加在向量y中第n个元素中。Step 4: Perform fast Fourier (FFT) transformation on the sub-data blocks x k (i) (k=1, 2, ... 127) in turn, set the number of fast Fourier transform points to 2048, and set the number of fast Fourier transform points to 2048. The result is denoted as X k , which is a 2048×1-dimensional vector. Calculate the square of the modulus value of the nth (n = 1 , 2, .

步骤5:BD2-B3频点卫星导航信号的有效工作带宽B为20.46MHz,根据式(5)计算出可以将向量y划分为30个子带,用ym(m=1,2,…,30)表示向量y的第m个子带数据块。Step 5: The effective working bandwidth B of the BD2-B3 frequency satellite navigation signal is 20.46MHz. According to formula (5), it is calculated that the vector y can be divided into 30 sub-bands, using y m (m=1,2,...,30 ) represents the mth subband data block of the vector y.

步骤6:依次搜索子带数据块ym(m=1,2,…,30)中的最大值dm,搜索算法采用“冒泡”排序法,将30个子带中的最大值组成维数大小为30×1的向量d=[d1,d2,…,d30]T,上标T为转置运算符。Step 6: Search for the maximum value d m in the sub-band data blocks y m (m=1, 2, ..., 30) in turn. The search algorithm adopts the "bubble" sorting method, and the maximum value in the 30 sub-bands is composed of dimensions. A vector of size 30×1 d=[d 1 ,d 2 ,…,d 30 ] T , where the superscript T is the transpose operator.

步骤7:采用“冒泡”排序法搜索向量d中的最小值dmin,设噪声平均功率值Pnoise并初始化为0,设计数器J并初始化为0。依次判断向量y的每一个元素y(n)(n=1,2,...,2048)是否小于dmin,若小于dmin,则将y(n)在Pnoise中累加,计数器J计数加1,所有2048个元素判断完成后,计算Pnoise/J并更新Pnoise值。Step 7: Use the "bubble" sorting method to search for the minimum value d min in the vector d, set the average noise power value P noise and initialize it to 0, and set the counter J and initialize it to 0. Judging in turn whether each element y(n) (n=1,2,...,2048) of the vector y is less than d min , if it is less than d min , y(n) is accumulated in P noise , and the counter J counts Add 1, after all 2048 elements are judged, calculate P noise /J and update the P noise value.

步骤8:以Pnoise的两倍作为判决门限值yt进行弱谐波干扰检测,依次判断向量y的每一个元素y(n)(n=1,2,...,2048)是否大于yt,若y(n)>yt,则判决为在频点f(n)上存在干扰,按照式(8)计算弱干扰谐波频率f(n)并输出。至此,对第i通道中的弱谐波干扰的检测。Step 8: Use twice the P noise as the decision threshold y t to perform weak harmonic interference detection, and sequentially determine whether each element y(n) (n=1,2,...,2048) of the vector y is greater than y t , if y(n)>y t , it is judged that there is interference on the frequency point f(n), and the weak interference harmonic frequency f(n) is calculated and output according to formula (8). So far, the detection of weak harmonic interference in the i-th channel.

依次按照步骤2至步骤8完成对所有通道中弱谐波干扰的检测。Follow steps 2 to 8 in sequence to complete the detection of weak harmonic interference in all channels.

Claims (1)

1. A method for detecting weak harmonic interference signals in a satellite navigation anti-interference antenna system is characterized by comprising the following steps:
the method comprises the steps of firstly, collecting and storing digital signals output by an analog-to-digital converter of a satellite navigation anti-interference antenna with a set time length of T milliseconds under the condition of no external electromagnetic interference, and storing the number L of data points in each corresponding channel as T multiplied by Fs×103Wherein F issSampling frequency for the analog-to-digital converter;
assuming that the satellite navigation anti-interference antenna system comprises M channels, the acquired and stored data form a matrix with dimension L multiplied by M, and the ith column of data of the matrix is marked as x (i) ([ x)0,x1,…,xL-1]T
Secondly, dividing the data vector x (i) into sub-data blocks which are overlapped with each other, wherein the length of each sub-data block is N, the value of N is set to be the positive integer power of 2, the overlapping rate between two adjacent sub-data blocks is set to be 50%, and the total number of the sub-data blocks is
Figure FDA0001531420200000011
K (k is 1, 2)… K) sub-data blocks denoted xk(i);
Thirdly, constructing a vector y with the size of Nx 1 dimension, and initializing each element in y to be 0, wherein y is represented as0=0;
Fourthly, sequentially sub-data blocks xkPerforming fast Fourier transform, setting the number of fast Fourier transform points to be N, and recording the result of the fast Fourier transform as Xk,XkIs a vector of dimension Nx 1; calculating XkThe nth element X in the vectorkThe squares of the modulus values of (n) are summed up in the nth element of the vector y, yk(n)=yk-1(n)+|Xk(n)|2,n=1,2,...,N;
Fifthly, dividing the vector y into S sub-bands according to the effective working bandwidth B of the satellite navigation system,
Figure FDA0001531420200000012
Fsfor sampling frequency, use ysThe S-th subband data block, S-1, 2, …, S, representing vector y;
sixthly, the sub-band data block y is searched in sequencesMaximum value of dsThe maximum values in the S subbands are combined into a vector d ═ d of size S × 11,d2,…,dS]T
Seventhly, searching the minimum value d in the vector dminLet the noise mean power value PnoiseAnd initialized to 0, a counter J is designed and initialized to 0; sequentially judging whether each element y (n) of the vector y is smaller than dminIf it is less than dminThen y (n) is added to PnoiseAnd (4) performing middle accumulation, adding 1 to the count of the counter J, and calculating P after judging all N elementsnoiseA combination of J and PnoiseUpdating the value;
eighth step with PnoiseIs twice as the decision threshold value ytCarrying out weak harmonic interference detection, and sequentially judging whether each element y (n) of the vector y is larger than ytIf y (n) > ytIf yes, the decision is at the frequency point
Figure FDA0001531420200000021
There is interference and f (n) is output.
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