Fault tolerant control of satellite formation flying using second order sliding mode control

Authors

M. Saif, Simon Fraser University
B. Ebrahimi, Ministry of Science, Research and Technology Islamic Republic of Iran
M. Vali, University of Kashan

Document Type

Conference Proceeding

Publication Date

12-23-2011

Publication Title

Conference Proceedings - IEEE International Conference on Systems, Man and Cybernetics

First Page

2015

Keywords

Fault tolerant control, satellite formation flying, second order sliding mode control, twisting algorithm

Last Page

2020

Abstract

Twisting, second order sliding mode control is presented to accommodate the thruster faults in the nonlinear MIMO picosatellite formation flying system with unknown time-varying disturbances. Robustness and stability of the proposed scheme is proved using twisting algorithm and its capability for formation keeping demonstrated against periodic thruster faults and external disturbances through simulations. © 2011 IEEE.

DOI

10.1109/ICSMC.2011.6083968

ISSN

1062922X

ISBN

9781457706523

Recommended Citation

Saif, M.; Ebrahimi, B.; and Vali, M.. (2011). Fault tolerant control of satellite formation flying using second order sliding mode control. Conference Proceedings - IEEE International Conference on Systems, Man and Cybernetics, 2015-2020.
https://scholar.uwindsor.ca/electricalengpub/336