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

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. Th...

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Main Authors: Ban, Ying Siang, Varatharajoo, Renuganth
Format: Article
Language:English
Published: Trans Tech Publications 2012
Online Access:http://psasir.upm.edu.my/id/eprint/23145/
http://psasir.upm.edu.my/id/eprint/23145/1/Optimal%20control%20for%20combined%20energy%20storage%20and%20attitude%20control%20system%20%28CEACS%29%20in%20small%20satellites.pdf
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author Ban, Ying Siang
Varatharajoo, Renuganth
author_facet Ban, Ying Siang
Varatharajoo, Renuganth
author_sort Ban, Ying Siang
building UPM Institutional Repository
collection Online Access
description 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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institution Universiti Putra Malaysia
institution_category Local University
language English
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publishDate 2012
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spelling upm-231452015-12-07T03:06:11Z http://psasir.upm.edu.my/id/eprint/23145/ Optimal control for combined energy storage and attitude control system (CEACS) in small satellites Ban, Ying Siang Varatharajoo, Renuganth 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. Trans Tech Publications 2012 Article PeerReviewed application/pdf en http://psasir.upm.edu.my/id/eprint/23145/1/Optimal%20control%20for%20combined%20energy%20storage%20and%20attitude%20control%20system%20%28CEACS%29%20in%20small%20satellites.pdf 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 http://www.scientific.net/AMM.110-116.3587 10.4028/www.scientific.net/AMM.110-116.3587
spellingShingle Ban, Ying Siang
Varatharajoo, Renuganth
Optimal control for combined energy storage and attitude control system (CEACS) in small satellites
title Optimal control for combined energy storage and attitude control system (CEACS) in small satellites
title_full Optimal control for combined energy storage and attitude control system (CEACS) in small satellites
title_fullStr Optimal control for combined energy storage and attitude control system (CEACS) in small satellites
title_full_unstemmed Optimal control for combined energy storage and attitude control system (CEACS) in small satellites
title_short Optimal control for combined energy storage and attitude control system (CEACS) in small satellites
title_sort optimal control for combined energy storage and attitude control system (ceacs) in small satellites
url http://psasir.upm.edu.my/id/eprint/23145/
http://psasir.upm.edu.my/id/eprint/23145/
http://psasir.upm.edu.my/id/eprint/23145/
http://psasir.upm.edu.my/id/eprint/23145/1/Optimal%20control%20for%20combined%20energy%20storage%20and%20attitude%20control%20system%20%28CEACS%29%20in%20small%20satellites.pdf