导弹迎击时飞机的最佳逃逸策略研究  

Optimal Escape Strategy of Fighter against Oncoming Missiles

作　　者：王斯财[1] 南英[2] 刘经纬[3] 

机构地区：[1]南昌航空大学航机学院,江西南昌330063 [2]南京航空航天大学航天学院,南京210016 [3]上海飞机设计研究所,上海200232

出　　处：《航空兵器》2009年第4期28-32,共5页Aero Weaponry

基　　金：南昌航空大学学校创新基金

摘　　要：研究了飞机在被导弹迎面攻击时的最佳逃逸策略。首先建立了弹-机追逃对抗飞行数学模型,提出了几种突防方案,即机动变轨技术、抛射诱饵以及综合这两种突防方案,通过大量飞行数值仿真直观地比较了各种突防策略,得出了飞机躲避导弹袭击的最佳策略——作非常规机动并且同时发射诱饵弹。The optimal escape strategy of the fighter vehicle against oncoming missile is studied. Firstly, the escape-intercept mathematic model of fighter vehicle and missile is built, and several escape strategies are presented, such as trajectory maneuver, bait technology and integration of both the two pen- etration strategies. Based on a great deal of flight numerical simulation, all kinds of penetration maneuver strategies are compared, and the optimal escape strategy is gotten for fighter escaping from the intercept of missile, that is integrating both trajectory maneuver and bait technology.

关 键 词：最佳逃逸策略 追逃对抗飞行 非常规机动 数值仿真 

分 类 号：V271.4[航空宇航科学与技术—飞行器设计]