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    Title :

    Optimal Attitude Control of Flexible Spacecraft with Minimum Vibration



    Conference:

    Conference, Guidance, navigation and control ; 2010 ; Toronto, Canada



    Publication date :

    2010-01-01


    Size :

    16 pages


    Remarks:

    Includes bibliographical references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English






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