Attitude fault tolerant control for satellite under actuator fault and inertial sensor fault

被引：0
|
作者：
Yang, Wenbo [1 ,2 ]
Wang, Jianjun [1 ]
Li, Shaoyuan [2 ,3 ]
Wang, Liandong [1 ]
机构：
[1] Shanghai Polytech Univ, Shanghai 201209, Peoples R China
[2] Minist Educ, Key Lab Syst Control & Informat Proc, Shanghai 200240, Peoples R China
[3] Shanghai Jiao Tong Univ, Dept Automat, Shanghai 200240, Peoples R China
来源：
PROCEEDINGS OF THE 39TH CHINESE CONTROL CONFERENCE | 2020年
关键词：
Attitude control; Actuator fault; Inertial sensor fault; Fault tolerant control;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Firstly, an adaptive sliding mode fault tolerant controller is designed for the satellite attitude control system aiming at unnormal outputs of control torques because of actuator fault, and the stability of the closed-loop system is analyzed by Lyapunov method. On this basis, considering the coincidence of the actuator fault and the inertial sensor fault with the unknowable attitude angular velocity of the satellite, corresponding fault tolerant controller is presented and the stability of the closed-loop system is analyzed. Finally, the numerical simulation results verify the effectiveness of the designed fault tolerant controller.
引用
收藏
页码：3439 / 3443
页数：5
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