Cover Image

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...

Full description

Saved in:
Bibliographic Details
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/23145/1/Optimal%20control%20for%20combined%20energy%20storage%20and%20attitude%20control%20system%20%28CEACS%29%20in%20small%20satellites.pdf
http://psasir.upm.edu.my/id/eprint/23145/
http://www.scientific.net/AMM.110-116.3587
Tags: Add Tag
No Tags, Be the first to tag this record!
id my.upm.eprints.23145
record_format eprints
spelling my.upm.eprints.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
institution Universiti Putra Malaysia
building UPM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Putra Malaysia
content_source UPM Institutional Repository
url_provider http://psasir.upm.edu.my/
language English
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.
format Article
author Ban, Ying Siang
Varatharajoo, Renuganth
spellingShingle Ban, Ying Siang
Varatharajoo, Renuganth
Optimal control for combined energy storage and attitude control system (CEACS) in small satellites
author_facet Ban, Ying Siang
Varatharajoo, Renuganth
author_sort Ban, Ying Siang
title 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_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_sort optimal control for combined energy storage and attitude control system (ceacs) in small satellites
publisher Trans Tech Publications
publishDate 2012
url 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
http://psasir.upm.edu.my/id/eprint/23145/
http://www.scientific.net/AMM.110-116.3587
_version_ 1643827972210163712
score 13.211869

Similar Items