2-D Coherent Integration Processing and Detecting of Aircrafts Using GNSS-Based Passive Radar

被引:16
|
作者
Zeng, Hong-Cheng [1 ,2 ]
Chen, Jie [1 ,3 ]
Wang, Peng-Bo [1 ]
Yang, Wei [1 ]
Liu, Wei [4 ]
机构
[1] Beihang Univ, Sch Elect & Informat Engn, Beijing 100191, Peoples R China
[2] Univ Sheffield, Sch Math & Stat, Sheffield S10 2TN, S Yorkshire, England
[3] Collaborat Innovat Ctr Geospatial Technol, Wuhan 430079, Hubei, Peoples R China
[4] Univ Sheffield, Elect & Elect Engn Dept, Sheffield S1 3JD, S Yorkshire, England
基金
美国国家科学基金会;
关键词
Two-dimensional (2-D) coherent integration; Radon Fourier Transform; modified matched filter; aircraft detection; GNSS-based passive radar; RADON-FOURIER TRANSFORM; TARGET DETECTION; BISTATIC RADAR;
D O I
10.3390/rs10071164
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
Long time coherent integration is a vital method for improving the detection ability of global navigation satellite system (GNSS)-based passive radar, because the GNSS signal is not radar-designed and its power level is very low. For aircraft detection, the large range cell migration (RCM) and Doppler frequency migration (DFM) will seriously affect the coherent processing of azimuth signals, and the traditional range match filter will also be mismatched due to the Doppler-intolerant characteristic of GNSS signals. Accordingly, the energy loss of 2-dimensional (2-D) coherent processing is inevitable in traditional methods. In this paper, a novel 2-D coherent integration processing and algorithm for aircraft target detection is proposed. For azimuth processing, a modified Radon Fourier Transform (RFT) with range-walk removal and Doppler rate estimation is performed. In respect to range compression, a modified matched filter with a shifting Doppler is applied. As a result, the signal will be accurately focused in the range-Doppler domain, and a sufficiently high SNR can be obtained for aircraft detection with a moving target detector. Numerical simulations demonstrate that the range-Doppler parameters of an aircraft target can be obtained, and the position and velocity of the aircraft can be estimated accurately by multiple observation geometries due to abundant GNSS resources. The experimental results also illustrate that the blind Doppler sidelobe is suppressed effectively and the proposed algorithm has a good performance even in the presence of Doppler ambiguity.
引用
收藏
页数:21
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