Satellite-to-satellite tracking and orbit computation accuracy is evaluated on the basis of data obtained from near earth spacecraft via the geostationary ATS-6. The near earth spacecraft involved are Apollo-Soyuz, GEOS-3, and NIMBUS-6. In addition ATS-6 is being tracked by a new scheme wherein a single ground transmitter interrogates several ground based transponders via ATS-6 to achieve the precision geostationary orbits essential in satellite-to-satellite orbit computation. Also one way Doppler data is being recorded aboard NIMBUS-6 to determine the position of meteorological platforms. Accuracy assessments associated with the foregoing mission related experiments are discussed.


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    Titel :

    Satellite-to-satellite system and orbital error estimates


    Beteiligte:
    Schmid, P. E. (Autor:in) / Argentiero, P. D. (Autor:in) / Vonbun, F. O. (Autor:in)

    Kongress:

    Precision Time and Time Interval Conf. ; 1975 ; Greenbelt, MD, United States


    Erscheinungsdatum :

    1976-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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