空基动能拦截弹制导控制系统综述  

A Survey on Guidance and Control System for Airborne Kinetic Energy Interceptor

作　　者：巩冰[1] 肖增博[1] 雷虎民[2] 

机构地区：[1]中国人民解放军93507部队 [2]空军工程大学防空反导学院

出　　处：《航空兵器》2013年第6期17-23,共7页Aero Weaponry

摘　　要：弹道导弹在未来战争中具有很大的威胁,利用空基动能拦截弹拦截处于助推段飞行的弹道导弹是世界各国正在研发的先进拦截技术之一。系统地论述了空基动能拦截弹的发展现状,构建了弹道导弹助推段拦截的作战流程,分析了弹道导弹在助推段的飞行特性,探讨了动能拦截弹制导控制系统的研究进展,在此基础上,重点指出了动能拦截弹制导控制设计需要解决的一些问题。Ballistic missile can greatly threaten one nation＇ s safety during the future war. Using air- borne kinetic energy interceptor （AKEI） intercepts the ballistic missile in the boost phase become more and more popular all over the world. The development status of AKEI is introduced, and the engagement process for boost phase ballistic missile interception is explored. Then, the flight characteristics of ballis- tic missile during the boost phase are analyzed, and the research developments of guidance and control system of AKEI are emphatically discussed. Finally, some problems need to be solved for the guidance and control system design are pointed out.

关 键 词：空基动能拦截弹 弹道导弹 助推段拦截 制导控制 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程] V448.2[航空宇航科学与技术—飞行器设计]