The invention discloses a spacecraft docking device and a spacecraft ground docking method. The spacecraft docking device comprises a substrate; the plurality of lower butt joint blocks are arranged on the substrate, and at least two of the plurality of lower butt joint blocks are provided with ground butt joint auxiliary calibration interfaces; the plurality of upper butt joint blocks are suitable for being installed on a butt joint object, at least two of the plurality of upper butt joint blocks are provided with ground butt joint auxiliary calibration holes, and the plurality of upper butt joint blocks are suitable for being in butt joint with the plurality of lower butt joint blocks respectively; and the plurality of laser indicating devices are suitable for being detachably installed in the plurality of ground docking auxiliary calibration interfaces respectively, and the laser indicating devices are suitable for emitting indicating laser. The spacecraft docking device provided by the embodiment of the invention has the advantages of reducing the ground docking difficulty, improving the ground docking efficiency and the like.

    本发明公开了一种航天器对接装置和航天器地面对接方法,所述航天器对接装置包括:基板;多个下对接块,多个所述下对接块设在所述基板上,多个所述下对接块中的至少两个上设有地面对接辅助校准接口;多个上对接块,多个所述上对接块适于安装在被对接物上,多个所述上对接块中的至少两个上设有地面对接辅助校准孔,多个所述上对接块适于分别与多个所述下对接块对接;多个激光指示装置,多个所述激光指示装置适于分别可拆卸地安装在多个所述地面对接辅助校准接口内,所述激光指示装置适于发出指示激光。根据本发明实施例的航天器对接装置具有降低地面对接难度、提高地面对接效率等优点。


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    Titel :

    Spacecraft docking device and spacecraft ground docking method


    Weitere Titelangaben:

    航天器对接装置和航天器地面对接方法


    Beteiligte:
    LIANG BIN (Autor:in) / WANG XUEQIAN (Autor:in) / XU WENFU (Autor:in) / KANG SHIN KWAN (Autor:in) / TAN JUNBO (Autor:in) / CHEN ZHANG (Autor:in)

    Erscheinungsdatum :

    20.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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