The MAST Flight System as a test bed for large space structure control algorithms is discussed. An overview is given of the control system architecture. The actuators, the sensors, the control computer, and the baseline damping algorithm are discussed.


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    Title :

    MAST flight system dynamic performance


    Contributors:
    Davis, L. (author) / Hyland, D. (author) / Otten, T. (author) / Ham, F. (author)


    Publication date :

    1986-11-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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