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/).
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 -