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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    Titel :

    Doppler aided attitude determination for spin stabilized spacecraft


    Beteiligte:
    Han, D. (Autor:in) / McElrath, T. (Autor:in) / Taylor, T. (Autor:in) / Howell, D. (Autor:in) / Voth, C. (Autor:in)

    Kongress:

    13th AAS/AIAA Space Flight Mechanics Meeting


    Erscheinungsdatum :

    2003-02-09


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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