According to the orbit control speed increment estimation method suitable for the rendezvous and docking task of the lunar orbit, the initial speed increment required by orbit transfer is combined with different orbit control engine combination modes, meanwhile, the characteristics of instruction time delay, execution mechanism time delay and the like of different control systems are fully considered, and before orbit control is executed every time, the orbit control speed increment can be estimated to be more accurate. And the orbit control speed increment is accurately estimated. According to the orbit control task speed increment calculation method capable of meeting the high-precision orbit control requirement, the estimation calculation precision of the orbit control speed increment is improved, and it is ensured that a spacecraft can execute high-precision orbit control.

    本发明提供了一种适用于月球轨道交会对接任务的轨控速度增量预估方法,能够根据变轨所需初始速度增量结合不同轨控发动机组合模式,同时,充分考虑不同控制系统的指令时延、执行机构时延等特性,在每次执行轨控前,精确估计轨控速度增量。本发明可以满足高精度轨道控制要求的轨控任务速度增量计算方法,提高了轨控速度增量预估计算精度,确保航天器能够执行高精度轨控。


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    Title :

    Orbit control speed increment estimation method suitable for moon orbit rendezvous and docking task


    Additional title:

    适用于月球轨道交会对接任务的轨控速度增量预估方法


    Contributors:
    CHEN CHUNLIANG (author) / ZHAO YANG (author) / XING ZHUOYI (author) / ZOU LEYANG (author) / SHENG RUIQING (author) / ZHU SHUNJIE (author)

    Publication date :

    2022-04-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS