基于反辐射导引头空间分辨点的弹着点推算方法研究  

Research into The Calculating Method of Impact Point Based on Critical Position of Anti-radiation Seeker

作　　者：刘国彬 刘朋 王永海 贺方君 LIU Guo-bin;LIU Peng;WANG Yong-hai;HE Fang-jun(Luoyang Electronic Equipment Test Center of China,Mengzhou 454750,China)

机构地区：[1]中国洛阳电子装备试验中心,河南孟州454750

出　　处：《舰船电子对抗》2019年第1期79-82,共4页Shipboard Electronic Countermeasure

摘　　要：阐述了反辐射导弹在有源诱偏干扰情况下的末端攻击过程,建立了反辐射导弹临界分辨点后的运动模型,分析了采用闭环挂飞试验模拟反辐射导弹末端攻击过程的可行性,提出了闭环飞行过程中反辐射导引头空间分辨点的寻找方法,给出了模拟反辐射导弹弹着点外推方法,并检验了该方法的可行性。This paper describes the terminal attack course of anti-radiation missile (ARM) under the condition of active deceptive jamming,establishes the motion model of anti-radiation missile (ARM) after critical position,analyzes the feasibility simulating the terminal attack course of ARM by means of closed-loop flight test,puts forward the method to find the critial position of ARM seeker in the closed-loop flying,gives the calculating method to simulate the impact point of ARM,and validates the feasibility of this method.

关 键 词：反辐射导引头 空间分辨点 闭环挂飞试验 弹着点 

分 类 号：TN974[电子电信—信号与信息处理]