Orbit maneuver exhibits significant applications in formation flight, spacecraft information supporting and on-orbit servicing etc. In the paper, we pay more attention to analyze spacecraft's control domain under extra maneuver ability. According to emulate different direction velocity increment in different plane thrown to spacecraft, we analyze the variation of orbit parameters change with velocity increment. Furthermore, we give some conclusions which can provide theory foundation for the task of spacecraft information supporting and on-orbit servicing.


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    Title :

    Emulation and analysis of spacecraft control domain


    Contributors:
    Jia, Wang (author) / Shilu, Shen (author) / Si, Shen (author)


    Publication date :

    2014-08-01


    Size :

    268768 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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