大气层外拦截弹制导律设计与仿真  

Design and Simulation of Guidance Law for Exoatmospheric Interceptor

作　　者：黄宁[1] 董长虹[1] 

机构地区：[1]北京航空航天大学,北京100083

出　　处：《战术导弹技术》2008年第6期49-53,共5页Tactical Missile Technology

摘　　要：研究了地基动能杀伤拦截弹拦截低轨目标的制导方法.设计了对目标预测拦截点进行攻击的拦截弹飞行过程中的制导律,提出了一种确定目标预测拦截点及在拦截过程中修正预测拦截点的方法;通过仿真分析验证了方案的可行性.The guidance technique of intercepting low orbit targets by using land-based kinetic-kill interceptor is researched. The guidance law for the interceptor to attack a predicted intercept point of target was designed. The method of confirming the predicted intercept point and modifying the point on the intercept course is given. Simulations were done to analyze and demonstrate the effectivity of the guidance law.

关 键 词：中制导律 预测拦截点 仿真 

分 类 号：V448.232[航空宇航科学与技术—飞行器设计]