Kalman filtering techniques are combined with a semianalytical orbit generator to develop a sequential orbit determination algorithm. The algorithm is investigated for computational efficiency, accuracy, and radius of convergence by comparison with truth ephemerides and a Cowell special perturbations filters (GTDS). Test cases relevant to satellite navigation are examined.


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    Titel :

    Semiannalytical satellite theory and sequential estimation


    Beteiligte:
    Taylor, S. P. (Autor:in) / Cefola, P. J. (Autor:in)


    Erscheinungsdatum :

    01.10.1980


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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