Sliding Mode Controller for Satellite Attitude Stabilization Maneuver

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/).

Download article (PDF)

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  -