中远程空空雷达导弹的新机动规避方式的探索  

Exploration of A New Evasive Maneuver Mode for Medium and Long Range Air-to-air Radar Missile

作　　者：邵彦昊 朱荣刚 贺建良[1,2] 孔繁峨 SHAO Yanhao;ZHU Ronggang;HE Jianliang;KONG Fan’e(Science and Technology on Electro-Optic Control Laboratory,Henan Luoyang 471000,China;Luoyang Institute of Electro-Optical Equipment,AVIC,Henan Luoyang 471000,China)

机构地区：[1]光电控制技术重点实验室,河南洛阳471000 [2]洛阳电光设备研究所,河南洛阳471000

出　　处：《弹箭与制导学报》2020年第4期75-78,84,共5页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：针对在不可逃逸攻击区内部如何逃逸问题,建立了一种考虑导弹气动力因素的导弹-飞机的三维追逃模型,研究了不同条件下S机动、俯冲机动对导弹攻击距离的影响,以及切向机动对雷达信号的影响,并根据规避理论设计了不同的机动规避方式及其组合,对逃逸概率和脱靶量进行了仿真。结果表明,在导弹不可逃逸攻击区内部进行适当的规避机动,目标仍然有一定的概率逃脱,其中置尾俯冲最为有效。Aiming at the problem of how to escape from the non-escapable attack area,a missile-aircraft three-dimensional pursuit model considering missile aerodynamic factors is established.The influence of S maneuver and dive maneuver on missile attack range under different conditions and the influence of tangential maneuver on radar signal is studied.Based on the theory of avoidance,a non-escapable missile-aircraft three-dimensional pursuit model is designed.With the same maneuvering evasion mode and its combination,the escape probability and miss distance are simulated.The results show that the target still has a certain probability of escape when the maneuver is properly carried out in the missile′s non-escapable attack area,and tail dive is the most effective one.

关 键 词：空空导弹不可逃逸攻击区 机动规避 机载雷达 逃逸概率 脱靶量 

分 类 号：TJ765.4[兵器科学与技术—武器系统与运用工程]