A procedure to compute the integer ambiguity problem when a GPS receiver is used in a multiple antenna configuration attached to a rotating spacecraft is presented. The method is applied to a simulation of an experimental satellite which uses the GPS receiver for attitude determination.


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    Titel :

    Integer ambiguity resolution in GPS for spinning spacecrafts


    Beteiligte:
    Ferrando, C. (Autor:in) / Perez, A. (Autor:in) / Sanchez Pena, R.S. (Autor:in)


    Erscheinungsdatum :

    1999-10-01


    Format / Umfang :

    573736 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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