This report documents selected activities and results associated with the installation, validation, and flight evaluation of an FAA-owned Head-Up Display (HUD) research system as installed in a Boeing 727-100 FAA aircraft. Requisite installation, boresight, and flight validation activities, along with results obtained from a combined flight experience/flight evaluation exercise employing government pilots are presented. Pilot comments addressing HUD system performance, display symbology, control low responses, hardware implementation, and operational modes are addressed. The HUD, a one-of-a-kind flightpath oriented research HUD, was evaluated in both an inertial (INS) referenced mode and an airmass (AM) referenced mode. Overwhelmingly, there was a strong preference for the INS referenced HUD mode. (Author)


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    Titel :

    Installation, Validation, and Flight Evaluation of the Federal Aviation Administration's Head-Up Display System


    Beteiligte:
    B. C. Scott (Autor:in) / C. O. Masters (Autor:in) / J. J. Ryan (Autor:in) / A. T. Brazer (Autor:in) / R. S. Bray (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    187 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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