A mathematical model is reported for determination of satellite position, velocity, and attitude using landmark coordinates as observables. This model, although developed with respect to earth stabilized missions, Tiros-N and Nimbus-G in particular, is applicable to any earth stabilized satellite in general.


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    Titel :

    Utilization of landmark data in attitude/orbit determination


    Beteiligte:
    Siddalingaiah, H. (Autor:in) / Desai, P. S. (Autor:in)


    Erscheinungsdatum :

    01.08.1975


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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