摘要
研究了在空间拦截中导弹的脱靶量，并分析了影响脱靶量的因素。用逆系统方法求取了最优空间末制导律。
The miss distance in space interception is studied, and the factors affecting the miss distance are analyzed in the paper. An optimal space terminal guidance law is derived through the inverse system method.
出处
《导弹与航天运载技术》
1997年第4期5-13,共9页
Missiles and Space Vehicles
