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微进动弹道导弹目标雷达特征提取
引用本文:陈行勇,黎湘,郭桂蓉,姜斌.微进动弹道导弹目标雷达特征提取[J].电子与信息学报,2006,28(4):643-646.
作者姓名:陈行勇  黎湘  郭桂蓉  姜斌
作者单位:国防科技大学电子科学与工程学院,长沙,410073
摘    要:该文总结了弹道导弹目标雷达识别的研究现状,引入微进动和微RCS的概念,推导了进动锥体目标对雷达波的姿态角计算公式,分析了微RCS和姿态角的关系,使用进动锥体目标的微RCS序列估计目标进动参数和惯量比。以惯量比为特征,提出了识别弹头和诱饵的方法。最后给出了仿真结果。

关 键 词:弹道导弹  微进动  微RCS  惯量
文章编号:1009-5896(2006)04-0643-04
收稿时间:2005-03-31
修稿时间:2005-08-30

Radar Feature Extraction of Micro-precession Ballistic Missile Warhead
Chen Hang-yong,Li Xiang,Guo Gui-rong,Jiang Bin.Radar Feature Extraction of Micro-precession Ballistic Missile Warhead[J].Journal of Electronics & Information Technology,2006,28(4):643-646.
Authors:Chen Hang-yong  Li Xiang  Guo Gui-rong  Jiang Bin
Affiliation:Research Institute of Space Electronics;National University of Defense Technology; Changsha 410073; China
Abstract:In this paper, the development of radar identification of ballistic missile warhead is summarized. Conceptions of micro-precession and micro-RCS are introduced. The aspect angle expression of a precession target is derived, and the relationship between micro-RCS and aspect angle is analyzed. Then the precession parameters and inertia ratio are estimated with micro-RCS. Inertia ratio is then used to discriminate warheads and decoys. Finally, a simulation result is provided.
Keywords:Ballistic missile  Micro-precession  Micro-RCS  Inertia
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