摘要
为实现对反辐射无人机(ARUAV)末制导阶段飞行姿态的动态分析,基于比相被动导引头测向跟踪理论和反辐射无人机飞行控制原理,在分析末制导阶段导引头天线视场内诱饵数量变化对反辐射无人机攻击姿态调整影响的基础上,建立了多诱饵诱偏条件下的无人机攻击动态模型,并在想定条件下仿真分析了末制导阶段无人机姿态随天线视场范围内辐射源数量分离变化而变化的全过程。仿真分析结果证明了模型的正确性。
In order to realize the dynamic analysis of the flight attitude of anti-radiation unmanned aerial vehicle（ARUAV） in the phase of terminal guidance, based on the direction finding and track- ing theory of the phase-comparison passive ARUAV,this paper establishes the dynam analyzing the influence of decoys quantity c nal guidance on attack attitude adj UAV attitude changes with the ch minal guidance in the condition of sults prove the correctness of the radar seeker （PRS） and the flight control principle of ic model of ARUAV attack with multi-decoy based on hange in seeker antenna view field in the phase of termi ustment of ARUAV, simulates and al ange of radiation resource quantity se multi-decoy under some assumptions. model. nalyzes the whole process of paration in the phase of ter-
出处
《舰船电子对抗》
2012年第6期59-65,70,共8页
Shipboard Electronic Countermeasure
关键词
反辐射无人机
末制导
诱饵
anti-radiation unmanned aerial vehicle terminal guidance decoy
