Volume 42 Issue 12
Jan.  2014
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Chen Peng, Hao Shiqi, Zhao Nanxiang, Zhou Jianguo. Micro-doppler analysis of helicopter’s rotor blades[J]. Infrared and Laser Engineering, 2013, 42(12): 3259-3264.
Citation: Chen Peng, Hao Shiqi, Zhao Nanxiang, Zhou Jianguo. Micro-doppler analysis of helicopter’s rotor blades[J]. Infrared and Laser Engineering, 2013, 42(12): 3259-3264.

Micro-doppler analysis of helicopter’s rotor blades

  • Received Date: 2013-04-20
  • Rev Recd Date: 2013-05-10
  • Publish Date: 2013-12-25
  • Recently, the research of micro-Doppler effect provides a new approach for accurate target identification, which possess an important application prospect of helicopter detection, classification and recognition. In this paper, the radar scattering cross section was predicted with the physical optics method, and micro-Doppler model of a helicopter rotor blade was modified. Based on the model, the echo signal of double blades and three blades with different shape and rotating speed was calculated and micro-Doppler effect was analyzed with STFT. The results show that different quantity, height and rotating speed have different influence on the curve shape, amplitude and period of the micro-Doppler, and some reference for helicopter identification by micro-Doppler is provided.
  • [1] Chen V C, Li F Y, Ho S S, et al. Micro-Doppler effect in radar: phenomenon, model, and simulation study[J]. IEEE Transactions on Aerospace and Electronic Systems, 2006, 42(1): 2-21.
    [2] Chen V C. Analysis of radar micro-doppler signature with time-frequency transform[C]//Proc Statistical Signal and Array Processing, 2000: 463-466.
    [3] Chen V C, Li F Y. Analysis of Micro-Doppler signatures[J]. IEE Proc Radar Sonar Navig, 2003, 150(4): 271-276.
    [4] Chen V C. Time-Frequency signatures of Micro-Doppler phenomenon for feature extraction[C]//Proceedings of SPIE in Wavelet Applications VII, 2000: 220-226.
    [5] Sparr T, Krane B. Micro-Doppler analysis of vibrating targets in SAR[J]. Radar Sonar and Navigation,2003, 150(4): 277-283.
    [6] Wang wei. The research of the target recognition techniques based on the Micro-doppler features of the aircraft[D]. Nanjing: Nanjing University of Information Science and Engineering, 2012. (in Chinese) 王维. 基于微多普勒特征的空中目标识别技术研究[D]. 南京: 南京信息工程大学, 2012.
    [7] Liu Zengdong, Feng Weiwei, Liu Meijuan, et al. New type of Doppler modulating technology[J]. Infrared and Laser Engineering, 2005, 34(5): 557-559. (in Chinese) 刘增东, 凤巍巍, 刘美娟, 等. 一种新型的多普勒调制技术[J]. 红外与激光工程, 2005, 34(5): 557-559.
    [8] Zhang Haiyang, Zhao Changming, Yang Suhui. The methods of decreasing the phase noise influence in Micro-Doppler laser[J]. Acta Photonica Sinica, 2011, 40(5): 754-757. (in Chinese) 张海洋, 赵长明, 杨苏辉. 激光微多普勒探测系统中降低相位噪声影响的方法研究[J]. 光子学报, 2011, 40(5): 754-757.
    [9] Yang Yanling, Li Yanchao, Gao Long, et al. Numerical simulation of balanced heterodyne detection for coherent lidar[J]. Infrared and Laser Engineering, 2011, 40(10): 1919-1922. (in Chinese) 杨彦玲, 李彦超, 高龙, 等. 相干激光雷达平衡外差探测方法的数值仿真[J].红外与激光工程, 2011, 40(10): 1919-1922.
    [10] Chen Hangyong, Wang Yi, Chen Haijian. Micro-Doppler analysis and simulation of a helicopter target[J]. Electronic Information Warfare Technology, 2009, 11(6): 26-28. (in Chinese) 陈行勇, 王祎, 陈海坚. 直升机目标微多普勒分析和仿真[J]. 电子信息对抗技术, 2009, 11(6): 26-28.
    [11] Rassem R, Mahafza. Radar Systems Analysis and Design Using MATLAB[M]. 2nd ed. England: Chapman and Hall/CRC, 2008.
    [12] Chen V C. The Micro-Doppler Effect in Radar[M]. Boston: Artech House, 2011.
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Micro-doppler analysis of helicopter’s rotor blades

  • 1. State Key Laboratory of Pulsed Power Laser Technology (Electronic Engineering Institute),Hefei 230037,China;
  • 2. Anhui Province Key Laboratory of Electronic Restriction Technology,Hefei 230037,China

Abstract: Recently, the research of micro-Doppler effect provides a new approach for accurate target identification, which possess an important application prospect of helicopter detection, classification and recognition. In this paper, the radar scattering cross section was predicted with the physical optics method, and micro-Doppler model of a helicopter rotor blade was modified. Based on the model, the echo signal of double blades and three blades with different shape and rotating speed was calculated and micro-Doppler effect was analyzed with STFT. The results show that different quantity, height and rotating speed have different influence on the curve shape, amplitude and period of the micro-Doppler, and some reference for helicopter identification by micro-Doppler is provided.

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