摘要
本文研究了固体弹道导弹耗尽关机制导方法，提出了一种适用于无推力终止系统工作的固体弹道导弹．在要求能量随机耗尽条件下的混合制导模型，并进行仿真分析，论证了方案的可行性。
in this paper, an approach to depleted shutdown guidance for solid ballistic missile is described. The complex guidance mathematical model applying to solid ballistic missile without thrust ending system is given under the condition that the fuel is depleted randomly. And then, it's correctness is proved by simulation.
出处
《国防科技大学学报》
EI
CAS
CSCD
北大核心
1996年第3期35-39,共5页
Journal of National University of Defense Technology
