Proceedings of the 3rd International Conference on Mechanical Engineering and Intelligent Systems (ICMEIS 2015)

Sliding Mode Controller for Satellite Attitude Stabilization Maneuver

Authors
Licheng Feng, Xiaoqian Chen, Tao Sheng
Corresponding Author
Licheng Feng
Available Online August 2015.
DOI
10.2991/icmeis-15.2015.161How to use a DOI?
Keywords
Sliding mode control; rigid satellite; attitude control; Lyapunov method
Abstract

Attitude control system of the rigid satellite is a coupling and uncertain nonlinear system with multi-inputs and multi-outputs. This paper presents a sliding mode controller for the satellite attitude system with limited control input and external disturbances. The design strategy can guarantees that the closed-system is global asymptotic stable and realizes the requirements of the control input saturation. The control algorithm is model-independent and it performs effectively on restraining bounded external disturbances.

Copyright
© 2015, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the 3rd International Conference on Mechanical Engineering and Intelligent Systems (ICMEIS 2015)
Series
Advances in Engineering Research
Publication Date
August 2015
ISBN
10.2991/icmeis-15.2015.161
ISSN
2352-5401
DOI
10.2991/icmeis-15.2015.161How to use a DOI?
Copyright
© 2015, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

TY  - CONF
AU  - Licheng Feng
AU  - Xiaoqian Chen
AU  - Tao Sheng
PY  - 2015/08
DA  - 2015/08
TI  - Sliding Mode Controller for Satellite Attitude Stabilization Maneuver
BT  - Proceedings of the 3rd International Conference on Mechanical Engineering and Intelligent Systems (ICMEIS 2015)
PB  - Atlantis Press
SP  - 854
EP  - 858
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmeis-15.2015.161
DO  - 10.2991/icmeis-15.2015.161
ID  - Feng2015/08
ER  -