This paper describes the theory of spin signature removal and the results obtained during the Genesis and Contour missions, during which spin axis pointing measurement errors of 1 degree or less were achieved.


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    Title :

    Doppler aided attitude determination for spin stabilized spacecraft


    Contributors:
    Han, D. (author) / McElrath, T. (author) / Taylor, T. (author) / Howell, D. (author) / Voth, C. (author)

    Conference:

    13th AAS/AIAA Space Flight Mechanics Meeting


    Publication date :

    2003-02-09


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





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