Sliding Mode Control for a Satellite Attitude Tracking System

摘要：

The main problem addressed is the attitude tracking control of rigid satellite in the presence of inertia matrix uncertainty and external disturbances. A sliding mode controller with PID sliding surface is presented. A detail stability analysis of the close loop system is include, and while there exists uncertainty in satellite inertia parameters or external disturbance, this control scheme has global stability and robustness. Simulations are performed for the satellite attitude control system. Simulation results demonstrate that the control scheme realizes the attitude tracking control and is robust to parametric uncertainty and to external disturbance torques.

作者: Dai Gao Jianting Lv

作者单位: School of Astronautics,Harbin Institute of Technology School of Astronautics,Harbin Institute of Technology;School of Mathematical Science,Heilongjiang Un

会议类型: 国际会议

会议名称: The 2nd International Symposium on Systems and Control in Aeronautics and Astronautics(第二届航空航天系统与控制国际会议 ISSCAA 2008)

会议地点: 深圳

会议语种:英文

页码: 953-956

在线出版日期: 2008-12-10（万方平台首次上网日期，不代表论文的发表时间）