The embodiment of the invention provides a satellite attitude control method and device based on a multi-flywheel array. The method comprises the following steps: acquiring a current attitude attribute value of a satellite; determining to adjust the attitude of the satellite according to the current attitude attribute value and a target attitude value; the current attitude attribute value and the target attitude value are input into a controller, target rotating speed adjustment values corresponding to all flywheels are obtained through the controller, the controller is arranged corresponding to all the flywheels in a flywheel array, and the flywheel array is distributed on all the shafts in multiple shafts. The embodiment of the invention provides a flywheel array satellite attitude control method based on multi-agent layered reinforcement learning.

    本申请实施例提供一种基于多飞轮阵列的卫星姿态控制的方法以及装置,所述方法包括:获取卫星的当前姿态属性值;根据所述当前姿态属性值与目标姿态值确认对所述卫星的姿态进行调整;将所述当前姿态属性值和所述目标姿态值输入控制器,通过所述控制器得到与各飞轮对应的目标转速调整值,其中,所述控制器是与飞轮阵列中各飞轮对应设置的,所述飞轮阵列分布在多轴中的各轴上。本申请的一些实施例提供一种基于多智能体分层强化学习的飞轮阵列卫星姿态控制方法。


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    Titel :

    Satellite attitude control method and device based on multi-flywheel array


    Weitere Titelangaben:

    一种基于多飞轮阵列的卫星姿态控制的方法以及装置


    Beteiligte:
    ZHAO JUNSUO (Autor:in) / YU JIALI (Autor:in) / WU FENGGE (Autor:in)

    Erscheinungsdatum :

    2022-07-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS




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