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弹载ESM系统中的目标方位及坐标解算
引用本文:宋新超.弹载ESM系统中的目标方位及坐标解算[J].舰船电子对抗,2012,35(2):62-65.
作者姓名:宋新超
作者单位:船舶重工集团公司723所,扬州,225001
摘    要:研究了基于弹载电子侦察(ESM)系统的测量方位与弹体空间三维坐标关系及变换原理,并根据测量方位与弹体姿态信息的解耦关系,得出目标相对于坐标原点的坐标及方位角和俯仰角。仿真结果表明,该方法可用于导引头侦察系统中目标方位的解算及定位。

关 键 词:弹载  电子侦察系统  坐标变换

Calculation of Target Direction and Coordinate in Missile-borne ESM System
SONG Xin-chao.Calculation of Target Direction and Coordinate in Missile-borne ESM System[J].Shipboard Electronic Countermeasure,2012,35(2):62-65.
Authors:SONG Xin-chao
Institution:SONG Xin-chao(The 723 Institute of CSIC,Yangzhou 225001,China)
Abstract:This paper studies the relationship and conversion principle between the measured directions based on missile-borne electronic support measure(ESM) system and missile-body space 3-D coordinate,deduces the target coordinate relative to the coordinate origin and azimuth,elevation according to the decoupling relationship between the measured direction and missile-body attitude information.The simulation results show that the method can be used for calculation and position of target direction in seeker reconnaissance system.
Keywords:missile-borne  electronic support measure system  coordinate conversion
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