The invention discloses a failure spacecraft attitude rapid adjustment method based on reinforcement learning, and the method comprises the steps: S1, building a failure spacecraft attitude mathematical model and a constraint model based on spacecraft attitude tail end constraint; s2, based on a Long-term performance index function in a reinforcement learning algorithm, establishing a judgment standard and a Critic network; and S3, on the basis of a Backstepping control framework, an Action network and the Critic network are combined, and an adaptive control method is established so as to control the failed spacecraft to enter a tail end constraint domain. According to the method, rapid attitude adjustment of the failed spacecraft before attitude motion evolution is realized, and a predetermined ignition maneuvering direction is entered.

    本发明公开了一种基于强化学习的失效航天器姿态快速调整方法,包括:步骤S1、基于航天器姿态末端约束,建立失效航天器姿态数学模型与约束模型;步骤S2、基于强化学习算法中的Long‑term性能指标函数,建立评判标准和Critic网络;步骤S3、基于Backstepping控制框架结合Action网络和所述Critic网络,建立自适应控制方法,以控制失效航天器进入末端约束域。本发明实现失效航天器在姿态运动演化前的快速姿态调整,进入预定点火机动指向。


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    Titel :

    Failure spacecraft attitude adjustment method based on reinforcement learning


    Weitere Titelangaben:

    一种基于强化学习的失效航天器姿态调整方法


    Beteiligte:
    HUANG JING (Autor:in) / MENG YIZHEN (Autor:in) / TIAN LULU (Autor:in) / SUN JUN (Autor:in) / ZHU DONGFANG (Autor:in)

    Erscheinungsdatum :

    2023-04-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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