摘要
通过全程拦截弹道的设计与计算,验证了与空间目标直接碰撞的可能性,对末制导做了分析与计算.分析并比较了几种较为典型的末制导规律,通过理论分析与大量实际的末制导段弹道计算,分别为单轴和三轴拦截器选择了末制导律;按选定的末制导律,进行了各种交会情形下的弹道计算.结果证明:如果不考虑控制误差,在0°～90°的各种交会角条件下计算的理论脱靶量均小于1m,能够实现直接碰撞击毁目标.
According to the design and analysis of global intercept trajectory, the possibility of straightly impacting space target is verified, and the terminal guidance is analysed and calculated. Several typical terminal guidance laws ate analysed and compared, and then two terminal guidance laws are chosed respectively for single-axis and three-axis interceptors by means of theory analysis and a lot of practical calculations of trajectory.It is shown that the direct impact can be realized to destroy the target if the control error is not considered and the theoretical missdistances are all less than lm under various intersection conditions(0°～90°).
出处
《战术导弹技术》
1992年第3期15-24,共10页
Tactical Missile Technology
关键词
末制导
碰撞
空间目标
拦截器
Terminal guidance
Collision
Space target
Interceptor
