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有终点交会角要求的拦截弹拦截导引设计
引用本文:邢立旦,陈万春,殷兴良.有终点交会角要求的拦截弹拦截导引设计[J].飞行力学,2007,25(4):37-39.
作者姓名:邢立旦  陈万春  殷兴良
作者单位:1. 北京航空航天大学,宇航学院,北京,100083
2. 中国航天科工集团,北京,100845
摘    要:针对终点处交会角固定的拦截导引问题,基于前人得到的需用速度公式,提出了通过迭代飞行时间来确定能满足交会角要求的需用速度,并在飞行过程中不断修正实际速度使其与需用速度一致的方法.该方法直观、可靠并能满足时空一致性的要求,最后通过仿真验证了其有效性.

关 键 词:交会角  飞行时间  需用速度
文章编号:1002-0853(2007)04-0037-03
收稿时间:2006-11-20
修稿时间:2007-05-25

Interception Guidance Design for Interceptor with Terminal Aspect Angle Constraint
XING Li-dan,CHEN Wan-chun,YIN Xing-liang.Interception Guidance Design for Interceptor with Terminal Aspect Angle Constraint[J].Flight Dynamics,2007,25(4):37-39.
Authors:XING Li-dan  CHEN Wan-chun  YIN Xing-liang
Abstract:To design the interception guidance with the terminal aspect angle constraint, based on the formula given by other persons, a new solution was brought out, which main idea was to obtain the needed velocity vector by iterating the flight time; then modify the practical velocity during the flight time until the needed and the practical velocities are almost equivalent. This method is intuitive and reliable, .and it can also guarantee that the target and the interceptor arrive at the same location at the same time. At last, the availability was demonstrated by the simulation example.
Keywords:aspect angle  flight time  needed velocity
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