DocumentCode :
3483471
Title :
A finite-time convergent continuous time sliding mode controller for spacecraft attitude control
Author :
Tiwari, Pyare Mohan ; Janardhanan, S. ; Nabi, Mashuq Un
Author_Institution :
Dept. of Electr. Eng., Indian Inst. of Technol. - Delhi, New Delhi, India
fYear :
2010
fDate :
26-28 June 2010
Firstpage :
399
Lastpage :
403
Abstract :
In this work a finite time convergent, continuous time sliding mode robust controller is proposed for attitude control of rigid spacecraft. The controller is designed with a new proposed fast terminal sliding mode (FTSM). Finite time reachability to the small neighborhood of sliding surface and faster finite time convergent of system states to equilibrium point is shown using a Lyapunov-type theorem. Simulation results show better convergent performance of the FTSM over terminal sliding mode controller (TSM).
Keywords :
Lyapunov methods; attitude control; continuous time systems; convergence; space vehicles; variable structure systems; Lyapunov type theorem; continuous time sliding mode controller; fast terminal sliding mode; finite time convergence; finite time reachability; spacecraft attitude control; Control systems; Convergence; Equations; Kinematics; Quaternions; Robust control; Sliding mode control; Space technology; Space vehicles; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Variable Structure Systems (VSS), 2010 11th International Workshop on
Conference_Location :
Mexico City
Print_ISBN :
978-1-4244-5829-5
Electronic_ISBN :
978-1-4244-5830-1
Type :
conf
DOI :
10.1109/VSS.2010.5544630
Filename :
5544630
Link To Document :
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