摘要
为提高反坦克导弹适应各类对抗环境的能力,提出了应用微分对策理论于导弹控制器设计的新思想;建立了导弹-坦克的微分对策模型,并对其进行了数值求解;此外,还讨论了如何将目标机动、导弹气动力变化等因素引入到导弹的飞行控制回路之中的问题;通常的经典反馈控制只能适应单一的飞行条件而不能满足导弹受控响应特性在飞行过程中变化很大的问题,提出了改善的途径,为研究导弹的智能控制飞行提供一些有用的参考数据。
In order to improve the ability of adaptation of anti-tank missiles in various gaming circumstances , a new concept employing the theory of differential games to the design of missile controls is presented . A missile - target differential game model is established and numerically solved . Various factors such as the introduction of maneuvering of the target and changes in aerodynamic forces on the missiles etc , aifecting the flight - control loop design, is discussed . As conventional feedback control can only adapt to a single condition of flight being thus unable to meet the multiplicity of missile control response characteristics in recurring in the course of flight , this proposal provides a way out, capable of suggesting useful data in intelligent control of missiles .
出处
《北京理工大学学报》
EI
CAS
CSCD
1991年第3期51-57,共7页
Transactions of Beijing Institute of Technology
关键词
导弹
反坦克导弹
攻防策略
missile
differential game / anti-tank missile
pursuit - evasion strategy