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中远距空空导弹导引头系统仿真及误差分析
引用本文:杨咪,张安,毕文豪,薛冰,黄平安.中远距空空导弹导引头系统仿真及误差分析[J].飞行力学,2020(1):66-72.
作者姓名:杨咪  张安  毕文豪  薛冰  黄平安
作者单位:西北工业大学航空学院;中国电子科技集团公司数据链技术重点实验室;西安飞机工业集团有限责任公司总师办
基金项目:国家自然科学基金资助(61573283);数据链技术重点实验室开放基金资助(CLDL-20182113)。
摘    要:针对中远距空空作战,建立了中远距空空导弹的飞行仿真模型,给出了导弹攻击目标的全过程,并给出了攻击结果,即脱靶量和目标杀伤概率的计算方法。在分析末制导阶段导弹雷达工作过程的基础上,分析了导引头误差对测量目标信息及导弹飞行过程和攻击结果的影响。最后,使用Visual Studio 2010和OpenGL进行了空空导弹的全过程飞行仿真,验证了模型的正确性和有效性。

关 键 词:中远距空空导弹  导引头误差  目标杀伤概率

Simulation and error analysis of medium-long-range air-to-air missile seeker system
YANG Mi,ZHANG An,BI Wenhao,XUE Bing,HUANG Pingan.Simulation and error analysis of medium-long-range air-to-air missile seeker system[J].Flight Dynamics,2020(1):66-72.
Authors:YANG Mi  ZHANG An  BI Wenhao  XUE Bing  HUANG Pingan
Institution:(School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China;Key Laboratory of Data Link Technology,CETC,Xi'an 710068,China;Office of Chief Engineer,Xi'an Aircraft Industry(Group)Company Ltd.,Xi'an 710089,China)
Abstract:For the medium-long-range air-to-air combat,the flight simulation model of medium-long-range air-to-air missile is specially established and the whole working process of a missile attacking a target is described.The method for calculating the attack results(i.e.,miss distance and the lethal probability)is given.By analyzing the working process of the missile radar in the terminal guidance phase,this paper analyzes the radar seeker error influencing on the target information,missile flight process and attack results.Finally,the Visual Studio 2010 and OpenGL are used to simulate the missile flight and validate the validity and correctness of the model.
Keywords:medium-long-range air-to-air missile  radar seeker error  lethal probability
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