Position and attitude control of formation flying satellites for restructuring their configurations by electromagnetic forces at the docking phase

Ayako Torisaka, Satoru Ozawa, Hiroshi Yamakawa, Nobuyuki Kobayashi

    研究成果

    11 被引用数 (Scopus)

    抄録

    This research proposes a relative position and attitude control method without reaction wheels, using magnetic force with multi-dipole for formation-flying spacecraft. This technology can be widely applied to re-configurable space structures that architect large structure, such like restructuring themselves by assembling basic structural units. One remarkable benefit is that this control method doesn't limit mission term because it never requires any types of fuel to drive RW for attitude control or unloading. So we focused on current control of dipoles which produce strong nonlinear magnetic forces and suggested a way of linearization of a nonlinear system for control by using reference controllable system. Also feasibility of this method and controllability were investigated, then the series of position and attitude control simulation were shown.

    本文言語English
    ホスト出版物のタイトルAIAA Guidance, Navigation, and Control (GNC) Conference
    出版ステータスPublished - 2013
    イベントAIAA Guidance, Navigation, and Control (GNC) Conference - Boston, MA
    継続期間: 2013 8 192013 8 22

    Other

    OtherAIAA Guidance, Navigation, and Control (GNC) Conference
    CityBoston, MA
    Period13/8/1913/8/22

    ASJC Scopus subject areas

    • 航空宇宙工学
    • 制御およびシステム工学
    • 電子工学および電気工学

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