The invention provides a satellite solar panel rotation control method, device and equipment and a storage medium, and relates to the technical field of satellite control. In some embodiments of the invention, a satellite comprises a satellite body and a solar panel, the satellite body is pivotally connected with a second rotating shaft, a first rotating shaft is mounted on the second rotating shaft, the first rotating shaft is connected with the solar panel, and an included angle of a true sun relative to an orbit of a satellite orbit is obtained; performing rotation control on the first rotating shaft and the second rotating shaft according to the absolute value of the included angle of the true sun relative to the orbit; the double-shaft control strategy is simple, the rotation angular speed is small, and the influence on satellite attitude control is reduced under the condition that the output energy of the solar panel is stable and sufficient.

    本公开提供一种卫星太阳帆板转动控制方法、装置、设备及存储介质,涉及卫星控制技术领域。在本公开的一些实施例中,卫星包括:卫星星体和太阳帆板,卫星星体与第二转轴枢转连接,第一转轴安装于第二转轴上,第一转轴与太阳帆板连接,获取卫星轨道的真太阳相对轨道的夹角;根据真太阳相对轨道的夹角的绝对值的大小,对第一转轴和第二转轴进行转动控制;本公开的双轴控制策略简单,转动角速度小,在太阳帆板输出能量稳定充足的情况下,降低对卫星姿态控制的影响。


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    Titel :

    Satellite solar panel rotation control method, device and equipment and storage medium


    Weitere Titelangaben:

    卫星太阳帆板转动控制方法、装置、设备及存储介质


    Beteiligte:
    ZHANG YONG (Autor:in) / LI JINGQI (Autor:in) / LIU CHEN (Autor:in) / HE QUAN (Autor:in) / RAO JIANBING (Autor:in) / CHEN YUHAN (Autor:in)

    Erscheinungsdatum :

    22.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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