DocumentCode :
1577548
Title :
Sliding mode controller design for rigid satellite attitude tracking
Author :
Wu, Shunan ; Sun, Zhaowei ; Li, Hui
Author_Institution :
Res. Center of Satellite Technol., Harbin Inst. of Technol., Harbin, China
fYear :
2009
Firstpage :
2238
Lastpage :
2243
Abstract :
The problem of attitude tracking control for rigid satellite is studied in this paper. Based on the dynamic equation and kinematics equation using error quaternion and error angular velocity, a sliding mode controller is initially designed to solve this problem. In order to avoid inherent chattering of sliding mode control and then improve control effect, a disturbance observer is introduced and included in the modified controller. The convergence of both controllers are respectively proved theoretically. Simulations are finally performed and the results demonstrate the performance of proposed controllers.
Keywords :
artificial satellites; attitude control; control system synthesis; observers; variable structure systems; disturbance observer; dynamic equation; error angular velocity; error quaternion; kinematics equation; rigid satellite attitude tracking control; sliding; sliding mode controller design; Angular velocity; Angular velocity control; Attitude control; Convergence; Equations; Error correction; Kinematics; Quaternions; Satellites; Sliding mode control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Robotics and Biomimetics (ROBIO), 2009 IEEE International Conference on
Conference_Location :
Guilin
Print_ISBN :
978-1-4244-4774-9
Electronic_ISBN :
978-1-4244-4775-6
Type :
conf
DOI :
10.1109/ROBIO.2009.5420472
Filename :
5420472
Link To Document :
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