The invention provides a checking method for determining a satellite orbit, and the method comprises the steps: dividing each on-orbit satellite into different types according to the orbit height of each on-orbit satellite, and determining the orbit determination result of each on-orbit satellite; the orbit determination result comprises a plurality of parameters; a plurality of parameters in the orbit determination result and a preset adjustable threshold are automatically checked through machine learning, and whether the orbit determination result meets the orbit determination precision requirement or not is judged; if the orbit determination result meets the orbit determination precision requirement, the orbit determination result is directly issued; if the orbit determination result does not meet the orbit determination precision requirement, continuing to perform the orbit determination optimization strategy, repeating the orbit determination and automatic check process of the satellite until the orbit determination result meets the orbit determination precision requirement, and continuing to complete the release process of the orbit determination result; or after the orbit determination optimization strategy cannot continuously solve the problem, manual processing is carried out. According to the invention, the time for determining a large number of satellite orbits and releasing products is shortened, and the operation benefit of a satellite orbit system is improved; and the workload of operators is reduced.

    本公开提出一种用于卫星轨道确定的检核方法,包括:根据各在轨卫星的轨道高度将每个在轨卫星划分为不同类别,并确定每个在轨卫星的定轨结果;定轨结果中包含多个参数;通过机器学习将定轨结果中的多个参数与预设可调门限进行自动检核,判断定轨结果是否符合定轨精度要求;若定轨结果符合定轨精度要求,则直接将定轨结果予以发布;若定轨结果不符合定轨精度要求,则继续进行定轨优化策略,重复进行卫星的定轨和自动检核过程,直至定轨结果符合定轨精度要求,继续完成定轨结果的发布过程;或定轨优化策略无法继续解决问题后转人工处理。本公开缩短了大数量卫星轨道确定及产品发布的时长,提高了卫星轨道系统的运行效益;减少了操作人员的工作量。


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    Title :

    Checking method for determining satellite orbit


    Additional title:

    一种用于卫星轨道确定的检核方法


    Contributors:
    XUE JIA (author) / WEI XIAOYING (author) / ZHANG HONG (author) / LI DONGLIN (author) / WANG JIANWEI (author) / SHI LEI (author) / YANG GUOCHANG (author) / LI QUANJUN (author) / XUE YONGTAI (author) / ZENG GUANG (author)

    Publication date :

    2023-03-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / G06N COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS , Rechnersysteme, basierend auf spezifischen Rechenmodellen



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