动能拦截临近空间飞行器的复合制导律设计  

Design of Compound Guidance Law for Kinetic Energy Intercepting Near Spacecraft

作　　者：安彬[1] 南英[1] 赵华超[2] 姬聪云 

机构地区：[1]南京航空航天大学航天学院,南京210016 [2]中国空空导弹研究院,河南洛阳471009

出　　处：《航空兵器》2017年第3期26-32,共7页Aero Weaponry

基　　金：航空科学基金项目(20140152002)

摘　　要：针对临近空间飞行器进行拦截,设计了一套复合制导律,并给出各制导段间的交班条件及参数设计。考虑临近空间飞行器典型的机动方式,对目标进行拦截仿真,对比分析了拦截弹采用复合制导律和比例制导律的仿真结果,以及交班对拦截的影响,实现了动能拦截临近空间飞行器。Aiming at intercepting near spacecraft,a compound guidance law is designed, and the hand-over conditions and parameter design of the guidance section are given. Considering the typical ma-neuvering mode of near spacecraft,the intercept simulation of the target is carried out. The simulation re-sults of the compound guidance law and the proportional guidance law are compared and analyzed,the in-tercept effect of the hand-over is got. Kinetic energy intercepting near spacecraft is achieved.

关 键 词：动能拦截 临近空间飞行器 复合制导律 交班条件 

分 类 号：TJ765.3[兵器科学与技术—武器系统与运用工程]