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.
Chattering free adaptive sliding mode control for attitude tracking of spacecraft with external disturbance
01.07.2014
381889 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Spacecraft Adaptive Sliding Mode Attitude Tracking Control Using DGCMG
British Library Conference Proceedings | 2012
|Adaptive integral sliding mode control for rigid spacecraft attitude tracking
Online Contents | 2013
|SAGE Publications | 2013
|