The invention discloses a multi-system coupled task guidance combination system which comprises a storage module and a task guidance module. Wherein the storage module is used for storing load parameters required in a task process. And the task guiding module is in communication connection with each module of the satellite and the load, and is used for receiving a task type injected on the ground, determining a whole device mode and a whole device sub-mode of the satellite according to the task type injected on the ground, further adjusting the attitude of the satellite according to a preset guiding law, and controlling the load according to the load parameter. Therefore, on-orbit autonomous task execution of the satellite is realized.

    本发明公开一种多系统耦合的任务导引联合系统,其包括存储模块以及任务导引模块。其中,存储模块用于存储任务过程中所需的载荷参数。任务导引模块与卫星的各个模块及载荷可通信地连接,用于接收地面上注的任务类型,并根据地面上注的任务类型,确定卫星的整器模式及整器子模式,进而根据预设的导引律调整卫星姿态,并根据所述载荷参数控制载荷,以实现卫星在轨自主执行任务。


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    Titel :

    Multi-system coupled task guidance combination system and method


    Weitere Titelangaben:

    一种多系统耦合的任务导引联合系统及方法


    Beteiligte:
    TANG TAO (Autor:in) / WU HUIYING (Autor:in) / WANG GUOHUA (Autor:in) / CHANG LIANG (Autor:in) / CHANG JIANPING (Autor:in) / CHEN HONGYU (Autor:in)

    Erscheinungsdatum :

    2022-11-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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