摘要
针对卫星姿态控制系统 ,建立了简化的线性数学模型 ,利用鲁棒控制方法设计了卫星姿态控制律 ,由于在设计中考虑了建模过程中的简化而带来的不确定性 。
Simplified linear mathematical model of satellite attitude control system is constructed, based on which attitude control law is designed using robust control theory. As simplifications in model construction are considered during design, the obtained control law based on simplified model is applicable to nonlinear satellite attitude system.
出处
《航天控制》
CSCD
北大核心
2001年第4期29-34,共6页
Aerospace Control
关键词
卫星
姿态控制
鲁棒控制
主动控制
Satellite\ Attitude control\ Robust control\ Active control
