The invention discloses a secondary unfolding flexible solar cell wing orbit injection autonomous step-by-step unfolding control method, which comprises the following steps of: performing orbit injection autonomous primary unfolding on a flexible solar cell wing, and performing secondary unfolding on the flexible solar cell wing after orbital transfer and butt joint actions of a spacecraft are completed; according to the method, the flexible solar cell wing can be autonomously unfolded step by step after entering the orbit, meanwhile, the fault mode is autonomously judged, the unfolding process is stopped, and the flexible solar cell wing and the spacecraft are protected.

    本发明公开了一种二次展开的柔性太阳电池翼入轨自主分步展开控制方法,包括:柔性太阳电池翼入轨自主一次展开,在航天器完成变轨、对接动作后,柔性太阳电池翼进行二次展开;本发明能够实现柔性太阳电池翼入轨后自主分步展开,同时自主判断故障模式并中止展开流程,对柔性太阳电池翼及航天器进行保护。


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    Titel :

    Autonomous step-by-step unfolding control method for orbit injection of secondary unfolding flexible solar cell wing


    Weitere Titelangaben:

    二次展开的柔性太阳电池翼入轨自主分步展开控制方法


    Beteiligte:
    XIAN KUICHENG (Autor:in) / NI XIAOFENG (Autor:in) / LI XUE (Autor:in) / HUO JIE (Autor:in) / CHENG LEI (Autor:in) / WANG ZHIYI (Autor:in) / PENG ZHILONG (Autor:in) / WANG WEI (Autor:in) / JIANG QIUXIANG (Autor:in) / YIN AIPING (Autor:in)

    Erscheinungsdatum :

    2023-09-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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