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

by Farhad Fani Saberi, Alireza Fazlyab, Abbas Ajorkar
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International Journal of Computer Applications
Foundation of Computer Science (FCS), NY, USA
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, Abbas Ajorkar . 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 ( July 2014), 28-34. DOI=10.5120/17270-7653

@article{ 10.5120/17270-7653,
author = { Farhad Fani Saberi, Alireza Fazlyab, Abbas Ajorkar },
title = { 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 },
issue_date = { July 2014 },
volume = { 98 },
number = { 16 },
month = { July },
year = { 2014 },
issn = { 0975-8887 },
pages = { 28-34 },
numpages = {9},
url = { https://ijcaonline.org/archives/volume98/number16/17270-7653/ },
doi = { 10.5120/17270-7653 },
publisher = {Foundation of Computer Science (FCS), NY, USA},
address = {New York, USA}
}
%0 Journal Article
%1 2024-02-06T22:26:55.024474+05:30
%A Farhad Fani Saberi
%A Alireza Fazlyab
%A Abbas Ajorkar
%T Design and Implementation of a Sliding Mode Attitude Controller of a Satellite in Software in the Loop Test Bed
%J International Journal of Computer Applications
%@ 0975-8887
%V 98
%N 16
%P 28-34
%D 2014
%I Foundation of Computer Science (FCS), NY, USA
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.

References
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Index Terms

Computer Science
Information Sciences

Keywords

Attitude Control Reaction wheel Satellite Sliding Mode Software in the loop

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