Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Optimal Attitude Control of Agile Spacecraft Using Combined Reaction Wheel and Control Moment Gyroscope Arrays


    Contributors:

    Conference:

    AIAA Modeling and Simulation Technologies Conference



    Publication date :

    2016-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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

    Doupe, Cole / Swenson, Eric D. / Cobb, Richard G. et al. | British Library Conference Proceedings | 2016



    Inertia-Free Spacecraft Attitude Control with Control Moment Gyroscope Actuation

    Agarwal, Kshitij / Weiss, Avishai / Kolmanovsky, Ilya et al. | AIAA | 2012


    Steering the Control Moment Gyroscope Clusters Onboard High-Agile Spacecraft

    Somov, Y. I. / Platonov, V. N. / Sorokin, A. V. et al. | British Library Conference Proceedings | 2004


    Inertia-Free Spacecraft Attitude Control with Control Moment Gyroscope Actuation

    Agarwal, K. / Weiss, A. / Kolmanovsky, I. et al. | British Library Conference Proceedings | 2012