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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    Titel :

    Adaptive attitude control of a flexible satellite


    Beteiligte:


    Erscheinungsdatum :

    2006-01-01


    Format / Umfang :

    1709881 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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    Magnetic Attitude Control of a Flexible Satellite

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