Paper Title:
Optimal Control for Combined Energy Storage and Attitude Control System (CEACS) in Small Satellites
  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. (Abstract)

  Info
Periodical
Chapter
Chapter 17: Precision Molding Processes
Edited by
Wu Fan
Pages
3587-3592
DOI
10.4028/www.scientific.net/AMM.110-116.3587
Citation
B. Y. Siang, R. Varatharajoo, "Optimal Control for Combined Energy Storage and Attitude Control System (CEACS) in Small Satellites", Applied Mechanics and Materials, Vols. 110-116, pp. 3587-3592, 2012
Online since
October 2011
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