The robust stabilization of the angular position of a spacecraft with dynamic elastic elements under dissipative properties is proposed. The control scheme is based on bang-bang control and linear output feedback. The former is based on minimum-time optimal control and the latter is designed with the invariant ellipsoid method. The control is achieved under uncertainty in the system and disturbances in the output measurements.


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    Title :

    Robust stabilization of a spacecraft with flexible elements using invariant ellipsoid technique


    Contributors:


    Publication date :

    2008


    Size :

    5 Seiten, 14 Quellen




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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