A differential GPS mechanization of an external data link concept under development at NASA Ames Research Center is discussed. The system is intended to evaluate the use of differential GPS to support helicopter approach operation. Analytical techniques for static testing and evaluation of the system hardware and software performance in real time are described. Several techniques that have been used to detect and rectify a specific problem encountered during the tests are dicussed. An example of flight test results using the validated system is provided.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Validating the airborne and ground based components of a differential GPS system


    Beteiligte:
    Edwards, F. G. (Autor:in) / Hegarty, D. M. (Autor:in) / Turner, R. N. (Autor:in) / Van Graas, F. (Autor:in) / Sharma, S. (Autor:in)

    Kongress:

    Institute of Navigation, National Technical Meeting ; 1988 ; Santa Barbara, CA, United States


    Erscheinungsdatum :

    1988-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    An Airborne Ground Penetrating Radar System

    Gregorwich, W. / IEEE; Aerospace and Electronics Systems Society | British Library Conference Proceedings | 1996


    Testing airborne electronic components

    Mintz, F. / Levine, M.B. | Engineering Index Backfile | 1955


    Airborne ground clutter measurement system design considerations

    Wicks, M. / Stremler, F. / Anthony, S. | IEEE | 1988


    Capabilities of Airborne and Ground Based Flight Simulation

    Markman, Steven R. | SAE Technical Papers | 1985