Abstract Orbit determination results are obtained for all IRS satellites by ISRO operational orbit determination software developed at ISRO Satellite Centre, Bangalore, using a batch least-squares estimator to process S-band range and range rate measurements. The orbit solutions are obtained through estimation of ballistic coefficient in addition to orbital parameters. A noteworthy improvement in orbit determination accuracy is noticed through this method. The position and velocity errors are in the range of 50 m to 80 m and 5 cm/s to 8 cm/s respectively.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    IRS Orbit Determination Accuracy Improvement


    Beteiligte:
    Vighnesam, N. V. (Autor:in) / Sonney, Anatta (Autor:in) / Subramanian, B. (Autor:in)


    Erscheinungsdatum :

    2002




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch



    Klassifikation :

    BKL:    55.60 Raumfahrttechnik
    Lokalklassifikation TIB:    770/7040



    IRS Orbit Determination Accuracy Improvement

    Vighnesam, N.V. | Online Contents | 2002


    IRS Orbit Determination Accuracy Improvement

    Vighnesam, N. V. / Sonney, Anatta / Subramanian, B. | Springer Verlag | 2002


    Erratum: IRS Orbit Determination Accuracy Improvement

    Vighnesam, N. V. / Sonney, Anatta / Subramanian, B. | Springer Verlag | 2003


    Erratum: IRS Orbit Determination Accuracy Improvement

    Vighnesam, N. V. / Sonney, Anatta / Subramanian, B. | Online Contents | 2003


    Errata: IRS Orbit Determination Accuracy Improvement

    Vighnesam, N.V. | Online Contents | 2003