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Optimal control for combined energy storage and attitude control system (CEACS) in small satellites


Citation

Ban, Ying Siang and Varatharajoo, Renuganth (2012) Optimal control for combined energy storage and attitude control system (CEACS) in small satellites. Applied Mechanics and Materials, 110-116. pp. 3587-3592. ISSN 1660-9336; ESSN: 1662-7482

Abstract

The combined energy storage and attitude control system (CEACS) combines both energy storage and attitude control modules via the flywheel technology. Previously only the conventional control methods were tested for CEACS. In this paper, H2 and H-infinity control methods are implemented in CEACS. The satellite attitude control performances show that both control options can be employed for a good attitude pointing accuracy.


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Official URL or Download Paper: http://www.scientific.net/AMM.110-116.3587

Additional Metadata

Item Type: Article
Divisions: Faculty of Engineering
DOI Number: https://doi.org/10.4028/www.scientific.net/AMM.110-116.3587
Publisher: Trans Tech Publications
Keywords: CEACS; Component; H infinity control; H2 control; Optimal control
Depositing User: Nabilah Mustapa
Date Deposited: 07 Dec 2015 03:06
Last Modified: 07 Dec 2015 03:06
Altmetrics: http://www.altmetric.com/details.php?domain=psasir.upm.edu.my&doi=10.4028/www.scientific.net/AMM.110-116.3587
URI: http://psasir.upm.edu.my/id/eprint/23145
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