有限时间绝对稳定的攻顶弹道设计  

Top Attack Trajectory Design Based on Finite-Time Stability

作　　者：王英焕 李锦[1] 张锐[1] WANG Ying-huan;LI Jin;ZHANG Rui(Beijing Institute of Electronic System Engineering, Beijing 100854, China)

机构地区：[1]北京电子工程总体研究所,北京100854

出　　处：《现代防御技术》2018年第2期57-61,105,共6页Modern Defence Technology

摘　　要：采用Lurie系统描述某反坦克导弹制导控制系统,给出系统剩余飞行时间与有限时间绝对稳定之间的描述,在此基础上进行该反坦克导弹全射程范围内(1~25 km)攻顶弹道设计,有效抑制了末端视线角发散,实现了对坦克类目标全射程范围内以40°~60°攻击角进行有效拦截。Lurie system is used to describe guidance control system of anti-tank missile. The description between missile flying time-to-go and finite-time stability is given,and on this basis the top attack trajectory within the whole range（ 1 ~ 25 km） is designed. The divergent angle of sight angle in the terminal guidance is effectively suppressed. The goal to effectively intercept tank by 40° ~ 60° attack angle within the whole range is reached.

关 键 词：LURIE系统 攻顶弹道 攻击角 反坦克导弹 制导控制 导引律 

分 类 号：TJ765.2[兵器科学与技术—武器系统与运用工程] TJ013