Dynamics model of a satellite with two solar panels is derived. It is assumed that solar panels are connected to central rigid body by two torsional flexible rods. A model reference adaptive controller is designed and its stability is proven by Lyapunov method. Capability of controller in an attitude maneuver by a numerical simulation is shown.


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    Title :

    Adaptive attitude control of a flexible satellite


    Contributors:


    Publication date :

    2006-01-01


    Size :

    1709881 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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