A Zero Notch Widening Method under High Dynamics

A zero-notch widening and high dynamic technology, applied in the field of satellite communication, can solve problems such as complex implementation process

Active Publication Date: 2021-07-06
SPACE STAR TECH CO LTD
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Problems solved by technology

The literature "Analysis of the Influence of Platform Motion on the Performance of Antenna Array in Satellite Navigation System" analyzes the influence of platform motion on the anti-jamming performance of the adaptive array. According to the characteristics of the machine, a statistically based space-time null widening method is proposed, but this method needs to multiply an expansion matrix on the basis of the original covariance matrix, and the implementation process is complicated

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  • A Zero Notch Widening Method under High Dynamics
  • A Zero Notch Widening Method under High Dynamics
  • A Zero Notch Widening Method under High Dynamics

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Embodiment Construction

[0033] Hereinafter, the present invention will be described in detail based on the drawings.

[0034] Such as figure 1 As shown, the present invention designs a zero-notching widening method under high dynamics, which is an improved QRD-SMI method of equal interval extraction, and can effectively enhance the robustness of filtering under high dynamic environments. The improved QRD-SMI method includes input data delay registration, data extraction, QR decomposition and real-time filtering, specifically including the following steps:

[0035] Step 1. Obtain the sampled data of the estimated covariance matrix of the received signal, perform bandpass filtering, Hilbert transform and amplitude-phase correction on the sampled data of the estimated covariance matrix, and enter step 2;

[0036] Step 2. After extracting the sampled data of the estimated covariance matrix at equal intervals, it is divided into two outputs, one of which is input to the FIFO module for storage, waiting f...

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Abstract

The present invention is a high dynamic null widening method, comprising: obtaining the sampling data of the received signal of the array antenna, performing band-pass filtering, Hilbert transform and amplitude-phase correction, extracting the obtained sampling data at equal intervals, and then outputting them in two channels, one of which is Input FIFO module storage, and the other channel is extracted at equal intervals, and then sent to the QR decomposition unit for covariance matrix estimation, and the updated covariance matrix is ​​output; forward iterative update of intermediate variables, according to the updated covariance matrix and intermediate variables Perform backward iterative calculations to obtain updated optimal weights; the sampled data of the estimated covariance matrix stored in the FIFO module is multiplied and added with the updated optimal weights, and then filtered and output. The invention equivalently expands the interference null, enhances the stability of filtering, and implements FPGA to enhance the stability of filtering.

Description

technical field [0001] The invention belongs to the technical field of satellite communication, and relates to a zero trap widening method under high dynamics. Background technique [0002] With the development and application of satellite communication technology, the problem of narrow-band or wide-band suppressive interference faced by its receivers has become increasingly prominent. Receivers based on array signal processing technology can adaptively eliminate these interferences by adjusting the weighted complex coefficients of each receiving array element. In engineering implementation, the LMS algorithm and the SMI algorithm are often used for adaptive filtering. The LMS algorithm is simple to implement and has a small amount of calculation. The engineering implementation was carried out earlier, but the convergence performance of the algorithm is greatly affected by the eigenvalue distribution of the correlation matrix. Therefore, the ability to suppress strong inter...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04B7/185H04L25/03
Inventor 张艳飞丁峰李晓青陈体军马世银王娇王春锋李容
Owner SPACE STAR TECH CO LTD
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