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
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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 |
| Statistic Details: | View Download Statistic |
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