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)


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    Titel :

    Optimal Control for Combined Energy Storage and Attitude Control System (CEACS) in Small Satellites



    Erschienen in:

    Applied Mechanics and Materials ; 110-116 ; 3587-3592


    Erscheinungsdatum :

    2011-10-24


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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