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2015•Advances in engineering research/Advances in Engineering ResearchOpen access

Sliding Mode Controller for Satellite Attitude Stabilization Maneuver

Licheng Feng, Xiaoqian Chen, Tao Sheng

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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.

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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.

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Available 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.

Key concepts: Control theory (sociology), Satellite, Attitude control, Mode (computer interface), Computer science, Controller (irrigation), Sliding mode control, Control engineering

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