The invention provides a sun-synchronous orbit moonlet electric propulsion orbit control autonomous planning method. According to the method, a mode of constructing a sub-satellite point trajectory of a satellite is adopted, a screening method of an autonomous orbit control starting moment is given in consideration of satellite charging requirements and avoiding of business conflicts, and an autonomous orbit control task planning method is designed in consideration of an electric propulsion orbit control capability and an on-board computer capability; autonomous orbit control may execute an expected number of orbit control services according to a plan. The solar synchronous orbit small satellite electric propulsion autonomous planning method has the advantages of being few in uploading instruction, simple in algorithm, small in calculation amount, accurate in result, high in anti-interference capacity and the like, meets the performance limitation of a spaceborne computer, and can autonomously run on a satellite.

    本发明提出太阳同步轨道小卫星电推进轨控自主规划方法。本发明采用构建卫星星下点轨迹的方式,考虑到卫星充电需求和避免业务冲突,给出自主轨控开始时刻的筛选方法,并且考虑电推进轨控能力和星载计算机能力,设计了自主轨控任务规划方法,自主轨控可按照规划执行期望次数的轨控业务。本发明所给出的太阳同步轨道小卫星电推进自主规划方法,具有上注指令少、算法简单、计算量小、结果准确、抗干扰能力强等优点,满足星载计算机的性能限制,能够在星上自主运行。


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    Title :

    Sun-synchronous orbit moonlet electric propulsion orbit control autonomous planning method


    Additional title:

    太阳同步轨道小卫星电推进轨控自主规划方法


    Contributors:
    LIU DONGCHEN (author) / CHOI WON BAEK (author) / FAN LINDONG (author) / HE XIAOJUN (author) / DAI LU (author) / REN HAO (author)

    Publication date :

    2024-03-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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