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    Title :

    Optimal Attitude Control of Agile Spacecraft Using Combined Reaction Wheel and Control Moment Gyroscope Arrays (AIAA 2016-0675)


    Contributors:

    Conference:

    AIAA Modeling and Simulation Technologies Conference 2016 ; 2016 ; San Diego



    Publication date :

    2016-01-01


    Size :

    23 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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