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    Titel :

    Fault-Tolerant Attitude Control Systems using Multi-Objective Optimization for a Spacecraft Equipped with Control Moment Gyros


    Beteiligte:
    Noumi, Ai (Autor:in) / Takahashi, Masaki (Autor:in) / Kanzawa, Takuya (Autor:in) / Haruki, Misuzu (Autor:in)

    Kongress:

    AIAA Guidance, Navigation, and Control Conference



    Erscheinungsdatum :

    01.01.2015




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Fault-Tolerant Attitude Control Systems using Multi-Objective Optimization for a Spacecraft Equipped with Control Moment Gyros (AIAA 2015-1088)

    Noumi, Ai / Takahashi, Masaki / Kanzawa, Takuya et al. | British Library Conference Proceedings | 2015



    Fault-Tolerant Attitude Control Systems for Satellite Equipped with Control Moment Gyros (AIAA 2013-5119)

    Noumi, A. / Takahashi, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013



    Precision Attitude Control of Spacecraft with Control Moment Gyros

    Taniwaki, Shigemune / Ohkami, Yoshiaki | AIAA | 2006