A double-satellite formation satellite lightweight autonomous task planning and scheduling method based on multi-objective optimization realizes double-satellite formation satellite autonomous task planning and scheduling with optimal comprehensive efficiency on the basis of on-satellite constraints, and ensures high-precision inter-satellite pointing and inter-satellite spacing maintenance during long-term operation of double satellites. According to the invention, the space between two satellites, the execution capability of a satellite thruster and the like are taken as constraints, a task planning mathematical model is established, formation reference satellite scheduling and orbit/attitude control strategy generation are carried out based on multiple optimization targets, and on-satellite full-autonomous, lightweight and optimal-comprehensive-efficiency rapid autonomous task scheduling is realized.

    一种基于多目标优化的双星编队卫星轻量化自主任务规划与调度方法,该方法基于星上约束,实现了综合效能最优的双星编队卫星自主任务规划与调度,保证双星长期运行期间的高精度星间指向和星间距保持。本申报专利以双星间距及卫星推力器执行能力等作为约束,建立任务规划数学模型,基于多优化目标进行编队基准星调度及轨道/姿态控制策略生成,实现了星上全自主、轻量化、综合效能最优的快速自主任务调度。


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    Titel :

    Double-satellite formation satellite lightweight autonomous task planning and scheduling method based on multi-objective optimization


    Weitere Titelangaben:

    一种基于多目标优化的双星编队卫星轻量化自主任务规划与调度方法


    Beteiligte:
    WANG LIJIAO (Autor:in) / LIU QIRUI (Autor:in) / LIU YIWU (Autor:in) / GUAN BIN (Autor:in) / LI YI (Autor:in) / LIN LIN (Autor:in) / LI YAN (Autor:in) / GAO YONG (Autor:in)

    Erscheinungsdatum :

    06.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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