针对大气层外拦截中段采用耗尽关机固体燃料发动机的情况，设计了基于零控脱靶量的鲁棒中制导律。
A midcourse guidance law for an exoatmospheric interceptor with solid engine, which has a significant ballistic coast to the endgame after burnout, is put forward.
针对大气层外高速飞行的动能拦截器，描述了末制导段拦截器的六自由度运动学方程。
Six-degree of freedom equations are described for high-speed interceptor flying in extra-atmospheric space.
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