The invention provides an autonomous fixed star observation method for an ultra-low orbit satellite. The autonomous fixed star observation method comprises the following steps: setting a whole satellite mode word; according to the whole satellite mode word, judging whether an autonomous working condition triggering enabling mark is enabled or not: if so, judging an orbit height to determine a working condition, and starting a fixed star observation task according to the working condition; and if prohibited, setting a working condition through a ground instruction, and starting a fixed star observation task according to the working condition. Meanwhile, the invention provides an autonomous fixed star observation system for the ultra-low orbit satellite. The mechanism meets the requirement of a fixed star observation task under the ultra-low orbit height condition, and the problems of large aerodynamic disturbance torque under the ultra-low orbit condition and large rotating torque caused by maneuvering of a rotary table can be solved; the ultra-low orbit fixed star observation working condition can be automatically switched according to the orbit height, and errors caused by ground orbit forecasting are reduced; meanwhile, the capability of intervening the whole satellite task on the ground is reserved, and whole satellite autonomous observation and ground forced observation can be switched at any time.

    本发明提供了一种用于超低轨卫星的自主恒星观测方法,包括:设置整星模式字;根据所述整星模式字,判断自主工况触发使能标志是否为使能:如果使能,则判断轨道高度决定工况,并根据工况,开始恒星观测任务;如果禁止,则通过地面指令设置工况,并根据工况,开始恒星观测任务。同时提供了一种用于超低轨卫星的自主恒星观测系统。本发明适应超低轨道高度条件下恒星观测任务要求,能够克服超低轨条件下大的气动干扰力矩,和转台机动时带来的较大转动力矩的问题;能够根据轨道高度自主切换超低轨恒星观测工况,减少了地面轨道预报带来的误差;同时保留了地面干预整星任务的能力,可随时切换整星自主观测和地面强制观测。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Autonomous fixed star observation method and system for ultra-low orbit satellite


    Weitere Titelangaben:

    用于超低轨卫星的自主恒星观测方法及系统


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

    Erscheinungsdatum :

    2023-12-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Orbit maintaining method of ultra-low orbit satellite

    XU MING / ZUO XIAOYU / ZHENG YARU et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Autonomous guidance method for recoverable aircraft carried on ultra-low orbit satellite platform

    GAO XUDONG / LI PENGJIE / XIE CHENGQING et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Linked Autonomous Interplanetary Satellite Orbit Navigation

    Parker, Jeffrey S. / Anderson, Rodney L. / Born, George H. et al. | NTRS | 2013


    Intelligent orbit maintenance control method and system for ultra-low orbit satellite

    ZHANG DAWEI / WANG ZIJUN / YANG SHENGQING et al. | Europäisches Patentamt | 2023

    Freier Zugriff