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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    Title :

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



    Published in:

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


    Publication date :

    2011-10-24


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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