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)
Optimal Control for Combined Energy Storage and Attitude Control System (CEACS) in Small Satellites
Applied Mechanics and Materials ; 110-116 ; 3587-3592
2011-10-24
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Optimal Control for Combined Energy Storage and Attitude Control System (CEACS) in Small Satellites
British Library Conference Proceedings | 2012
|A combined energy and attitude control system for small satellites
Elsevier | 2003
|A combined energy and attitude control system for small satellites
Online Contents | 2004
|The combined energy and attitude control system for small satellites-Earth observation missions
British Library Conference Proceedings | 2004
|