有源诱偏系统抗反辐射导弹动态飞行过程分析

Dynamic Flight Course Analysis of Radiation Source Decoy System Resist Anti-Radiation Missile

结合ARM的发射、攻击过程,重点对ARM飞行轨迹为多段弧线和直线相连接的复杂情况进行了分析,并推导出了误差修正圆弧段圆心的快速计算公式和航迹段交接位置的计算公式,最后通过计算机仿真与结果分析,得到了有源诱偏系统对抗反辐射导弹实用的布站间距配置方案,为设计和部署有源诱偏系统提供了理论依据。

Proceed with the launching and attack course of ARM,the complicated situation that the ARM＇s trajectory consists of many sections of arcs and straight lines has been especially analysed,and the formulas of error correction arc＇s center and the track intersection have been derived out.Through computer simulation and analysis of results,the practical configuration of the distance of radiant sources has been proposed.The conclusions have offered the theoretical foundation for designing and deploying and the radiation source decoy system.