A control scheme of artificial gravity based on the spinning tether system is proposed for manned long-term space mission in this paper. Firstly, the mathematical model of space tether system is established by Lagrangrian modeling method. Secondly, a passive deployment method is designed to realize the rapid deployment control of hundreds of meters short tether. Finally, to deal with the overload stability, a global fast terminal sliding mode controller is designed under the spinning of in-plane motion. The proposed artificial gravity scheme is validated by numerical analysis.


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    Titel :

    The tether-based artificial gravity construction and control for manned long-term space mission


    Beteiligte:
    Haochang, Tian (Autor:in) / Aijun, Li (Autor:in) / Hongshi, Lu (Autor:in) / Changqing, Wang (Autor:in)


    Erscheinungsdatum :

    2018-08-01


    Format / Umfang :

    792614 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Artificial Gravity for Long Duration Manned Space Flight

    Hoegenauer, E. / Wagner, K. R. / AIAA | British Library Conference Proceedings | 1994


    Artificial Gravity for Long Duration Manned Space Flight

    Hoegenauer, E. / Wagner, K. R. / AIAA | British Library Conference Proceedings | 1994


    Artificial gravity for long duration manned space flight

    Hoegenauer, E. / Wagner, K. | AIAA | 1994