A series of Global Positioning System (GPS) flight tests were performed on a National Aeronautics and Space Administration's (NASA's) Shuttle Training Aircraft (STA). The objective of the tests was to evaluate the performance of GPS-based navigation during simulated Shuttle approach and landings for possible replacement of the current Shuttle landing navigation aid, the Microwave Scanning Beam Landing System (MSBLS). In particular, varying levels of sensor data integration would be evaluated to determine the minimum amount of integration required to meet the navigation accuracy requirements for a Shuttle landing. Four flight tests consisting of 8 to 9 simulation runs per flight test were performed at White Sands Space Harbor in April 1991. Three different GPS receivers were tested. The STA inertial navigation, tactical air navigation, and MSBLS sensor data were also recorded during each run. C-band radar aided laser trackers were utilized to provide the STA 'truth' trajectory.


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    Titel :

    Results from a GPS Shuttle Training Aircraft flight test


    Beteiligte:
    Saunders, Penny E. (Autor:in) / Montez, Moises N. (Autor:in) / Robel, Michael C. (Autor:in) / Feuerstein, David N. (Autor:in) / Aerni, Mike E. (Autor:in) / Sangchat, S. (Autor:in) / Rater, Lon M. (Autor:in) / Cryan, Scott P. (Autor:in) / Salazar, Lydia R. (Autor:in) / Leach, Mark P. (Autor:in)


    Erscheinungsdatum :

    1991-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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