The CBERS-1 is the first Sun-synchronous orbit resource satellite cooperatively developed by China and Brazil. The CBERS-1 had been successfully launched into the designed orbit by the Chinese Long-March launch vehicle. It has been normally operated in the high-accuracy Sun-synchronous, recursive, frozen orbit designed for remote-sensing users through a series of orbit acquisition, sub-satellite-point trace acquisition and orbit maintenance manoeuvres. The paper briefly presents the mission objectives, system structure, orbit control strategy, control performance, flight software and on-orbit operations for the orbit control system of the CBERS-1, as well as its flight results.


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    Titel :

    Orbit acquisition and trajectory rendezvous control of CBERS-1


    Beteiligte:
    Wang Xudong, (Autor:in) / Li Xinfeng, (Autor:in) / Xi Dunyi, (Autor:in) / Ni Xingzhen, (Autor:in) / Yang Jiachi, (Autor:in) / Huang Fuming, (Autor:in) / Yang Xiaoqin, (Autor:in) / Tan Wei, (Autor:in) / Zhang Rongzhi, (Autor:in) / Li Jisheng, (Autor:in)


    Erscheinungsdatum :

    2000-01-01


    Format / Umfang :

    271261 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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