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    Title :

    Gain Scheduled Robust Attitude Control Law for Flexible Launchers Using Eigenstructure Assignment and Hinifnity Techniques


    Contributors:

    Conference:

    AIAA Guidance, Navigation, and Control Conference and Exhibit



    Publication date :

    2003-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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