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Design and Implementation of a Sliding Mode Attitude Controller of a Satellite in Software in the Loop Test Bed

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International Journal of Computer Applications
© 2014 by IJCA Journal
Volume 98 - Number 16
Year of Publication: 2014
Authors:
Farhad Fani Saberi
Alireza Fazlyab
Abbas Ajorkar
10.5120/17270-7653

Farhad Fani Saberi, Alireza Fazlyab and Abbas Ajorkar. Article: Design and Implementation of a Sliding Mode Attitude Controller of a Satellite in Software in the Loop Test Bed. International Journal of Computer Applications 98(16):28-34, July 2014. Full text available. BibTeX

@article{key:article,
	author = {Farhad Fani Saberi and Alireza Fazlyab and Abbas Ajorkar},
	title = {Article: Design and Implementation of a Sliding Mode Attitude Controller of a Satellite in Software in the Loop Test Bed},
	journal = {International Journal of Computer Applications},
	year = {2014},
	volume = {98},
	number = {16},
	pages = {28-34},
	month = {July},
	note = {Full text available}
}

Abstract

In this paper, a robust attitude control algorithm is developed based on sliding mode control for a satellite using four reaction wheels in a tetrahedron configuration. In this method, asymptotic stability of the proposed algorithm has been proven on lyapunov theory. Then, in order to evaluate the performance of the proposed algorithm, a low-cost real-time software in the loop test bed is provided. The presented test bed is capable of real-time assessing the attitude sliding mode control algorithm. In this test bed, real-time modeling of satellite dynamic, environmental disturbances and reaction wheels are achieved in a simulator computer and the proposed control algorithm performance is investigated by implementing it in an electronic control board of the software in the loop test bed.

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