摘要
针对数字式导弹姿态控制系统,通过对离散变结构控制的研究,提出了一种姿态控制系统的离散变结构控制方法,设计了变结构控制律。该变结构控制律在实现姿态控制系统鲁棒控制的同时,有效地抑制了传统变结构控制的抖振现象。仿真结果验证了本文方法的有效性。
Through researches of discrete variable structure(VS) control and digital missile attitude control system, a discrete VS control approach is proposed to be applied to the attitude control system .This VS control law implements robust control of attitude control system, at the same time, it overcomes the traditional chattering problem. This approach is validated effectively from the results of simulation.
出处
《导弹与航天运载技术》
北大核心
2006年第2期43-45,共3页
Missiles and Space Vehicles
关键词
姿态控制
导弹
离散
变结构
Attitude control
Missile
Discrete
Variable structure