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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    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


    Format / Umfang :

    11 Seiten, 30 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Integer ambiguity resolution in GPS for spinning spacecrafts

    Ferrando, C. / Perez, A. / Sanchez Pena, R.S. | IEEE | 1999



    APPLIED INTERVAL BASED INTEGER AMBIGUITY RESOLUTION

    van Kampen, E. | Online Contents | 2009


    ON THE RELIABILITY OF INTEGER AMBIGUITY RESOLUTION

    Verhagen, S. | Online Contents | 2005


    Real Time Attitude Independent GPS Integer Ambiguity Resolution

    Lightsey, E. Glenn / Crassidis, John L. | Online Contents | 2004