Chattering Free Adaptive Sliding Mode Control for Attitude Tracking of Spacecraft with External Disturbance
In this paper,the attitude tracking problem of spacecraft in the presence of unknown disturbance is investigated.By using the adaptive control technique and Lyapunov stability theory,a chattering free adaptive sliding mode control law is proposed for the attitude tracking problem of spacecraft with unknown disturbance.Simulation results are employed to demonstrate the effectiveness of the proposed control design technique in this paper.
Attitude Tracking Disturbance Sliding Mode Chattering Free
ZHANG Xuxi LIU Xianping
College of Science,Harbin Engineering University,Harbin 150001,P.R.China;College of Automation,Harbi College of Science,Harbin Engineering University,Harbin 150001,P.R.China
国际会议
The 33th Chinese Control Conference第33届中国控制会议
南京
英文
2224-2228
2014-07-28(万方平台首次上网日期,不代表论文的发表时间)