摘要
运用飞行力学原理和最优过程理论 ,在考虑导弹击顶攻击坦克有弹道倾角要求的条件下 ,推导出了一种适用于反坦克导弹击顶制导的组合性能指标最优的导引律。
Overhead attack guidance is a direction of accurate guidance for anti tank missiles. In this paper, the law of overhead attack guidance for anti tank missiles is studied applying principles of flight mechanics and theory of optimum proceses. An optimum guidance law that meets the overall performance index of overhead attack guidance for anti tank missiles is proposed to satisfy the requirements of ballistic inclined angle when missile attacks a tank. The result of simulation shows the validity of the guidance law.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
1999年第2期179-181,共3页
Acta Armamentarii
关键词
反坦克导弹
击顶制导律
最优导引律
制导律
anti-tank missile, overhead attack guidance, optimum guidance law, ballistic inclined angle
