摘要
本文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。利用非线性精确线性化理论设计了目标机动时的非线性末制导律。
The missdistance of missile in space interception is researched,and the factors affected the missdistance is analyzed in the paper.A nonlinear terminal guidance for maneuver targets is derived by nonlinear exact linearization.
出处
《宇航学报》
EI
CAS
CSCD
北大核心
1998年第2期37-42,共6页
Journal of Astronautics