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    Application of GPS Tracking Techniques to Orbit Determination for TDRS

    Application of GPS Tracking Techniques to Orbit Determination for TDRS


    In this paper, we evaluate two fundamentally different approaches to TDRS orbit determination utilizing Global Positioning System (GPS) technology and GPS-related techniques. In the first, a GPS flight receiver is deployed on the TDRSS spacecraft. The TDRS ephemerides are determined using direct ranging to the GPS spacecraft, and no ground network is required. In the second approach, the TDRSS spacecraft broadcast a suitable beacon signal, permitting the simultaneous tracking of GPS and TDRSS satellites from a small ground network. Both strategies can be designed to meet future operational requirements for TDRS-2 orbit determination.

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    Titel :

    Application of GPS Tracking Techniques to Orbit Determination for TDRS

    Beteiligte:
    B. J. Haines (Autor:in) / S. M. Lichten (Autor:in) / R. P. Malla (Autor:in) / S. C. Wu (Autor:in)
    Erscheinungsdatum :

    1993

    Format / Umfang :

    11 pages

    Medientyp :

    Report

    Format :

    Keine Angabe

    Sprache :

    Englisch

    Schlagwörter :

    Astronautics , Spacecraft Trajectories & Flight Mechanics , Unmanned Spacecraft , Navigation Systems , Global positioning system , Navigation satellites , Orbit calculation , Tdr satellites , Ephemerides , Rangefinding , Beacons , Broadcasting , Receivers

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