Hypersonic target TBD accumulation detection method through space-time polynomial radon transformation

A Radon transform and hypersonic technology, applied in the field of radar signal processing and data processing, can solve the problems that cannot fully meet the needs of inter-frame signal accumulation, prone to false alarms, and no distinction

Active Publication Date: 2016-06-29
NAVAL AVIATION UNIV
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Problems solved by technology

[0005] (1) The precondition of the traditional Hough transform TBD is that the target moves in a straight line, and its detection performance will decrease when the hypersonic target in the adjacent space moves along a curve;
[0006] (2) Most of the Hough transform TBD is accumulated in the Cartesian coordinate system. For hypersonic targets in the adjacent space, since the target is far away, the position error caused by the radar azimuth error will be very large, making the trajectory of the target in the Cartesian coordinate system The topological shape of the real trajectory is quite different, w

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[0067] Below in conjunction with accompanying drawing, describe technical solution of the present invention in detail, with reference to accompanying drawing figure 2 , concrete steps of the present invention include:

[0068] Step (1), extracting radar signals of K scan frames after radar signal processing, discretizing each signal, and obtaining a three-dimensional signal matrix s(m,n, k), where m represents the number of wave positions, m=1,2,...,M, M is the total number of wave positions, n represents the distance unit label of the echo signal, n=1,2,...,N,N is the total number of distance units, k represents the label of the scanning frame, k=1,2,...,K, and the elements in the matrix are the signal amplitudes corresponding to the detection unit;

[0069] Step (2), setting a preprocessing threshold, comparing each element s(m,n,1) in the signal matrix of the first frame with the first threshold, and finding a point greater than the first threshold;

[0070] Step (3), on...

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Abstract

The invention relates to a hypersonic target TBD accumulation detection method through space-time polynomial radon transformation and belongs to the field of radar signal processing and data processing.According to the characteristics that a hypersonic target of the near space is long in distance, ultra high in speed and high in accelerated speed, modeling is conducted on movement of a target azimuth dimension and a radial distance dimension with a polynomial, parameter research is conducted in the azimuth dimension and the radial distance dimension, and energy accumulation is achieved in a parameter space of space-time polynomial radon transformation.By means of the method, TBD accumulation is conducted under a polar coordinate system, the problems that a measuring trajectory topology is seriously deformed under a rectangular coordinate system, and it is difficult for the measuring path topology to be matched with a real trajectory are solved, accumulation is conducted by means of amplitude of signals, the accumulated error brought by radar signal binarization preprocessing conducted by a traditional TBD is avoided, the false-alarm probability is lowered, and real-time performance of detection is improved.

Description

technical field [0001] The invention belongs to the field of radar signal processing and data processing, and is suitable for solving the problem of TBD non-coherent signal accumulation of hypersonic stealth maneuvering targets. Background technique [0002] Hypersonic speed is more than Mach 5, which is more than 5 times the speed of sound (about 6000 kilometers per hour). Realizing hypersonic flight in the atmosphere is the most cutting-edge technology at present. The most famous one is the HTV-2 "Falcon" in the United States. Sonic aircraft program, X-37B aerospace demonstrator, X-43 and X-51 hypersonic demonstrator, etc. The high-altitude "corridor" 20 to 100 kilometers above the ground is an ideal space for hypersonic vehicles to fly long distances, also known as adjacent space. In this "corridor", the engine is briefly started to push the aircraft to climb again, fall back, and climb again, and so on. , making a "jump" every two minutes, each jump is about 450 kilomet...

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Application Information

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IPC IPC(8): G01S7/41
CPCG01S7/41
Inventor 吴巍王国宏谭顺成于洪波
Owner NAVAL AVIATION UNIV
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