摘要
针对最优鲁棒控制理论应用于导弹姿控系统设计中的原理缺陷,提出了导弹姿控系统设计中的变增益鲁棒控制方法.首先介绍了基于状态反馈的变增益鲁棒控制理论的基本原理,进而把它应用于姿控系统的设计并进行了仿真分析,之后就变增益鲁棒控制与最优鲁棒控制应用于导弹姿控系统的设计性能进行了比较分析,得出了一些有益的结论.
Aiming at the theory limitation of the optimal robust control in designing the missile attitude control system,the design method of missile attitude control system based on gain scheduling robust control is proposed.Firstly,the basic principle of gain scheduling robust control based on state feedback is introduced,attitude control system is designed,and simulation analysis is present.Secondly,the performance of which gain scheduling robust control and optimal robust control in designing missile attitude con...
出处
《战术导弹技术》
2010年第1期95-99,共5页
Tactical Missile Technology
关键词
变增益鲁棒控制
线性变参数
姿控系统
gain-scheduling robust control
linear parameter varying(LPV)
attitude control systems