Aircraft functional systems and crew systems were defined for a 1995 transport aircraft through a process of mission analysis, preliminary design, and evaluation in a soft mockup. This resulted in a revolutionary pilot's desk flight station design featuring an all-electric aircraft, fly-by-wire/light flight and thrust control systems, large electronic color head-down displays, head-up displays, touch panel controls for aircraft functional systems, voice command and response systems, and air traffic control systems projected for the 1990s. The conceptual aircraft, for which crew systems were designed, is a generic twin-engine wide-body, low-wing transport, capable of worldwide operation. The flight control system consists of conventional surfaces (some employed in unique ways) and new surfaces not used on current transports. The design will be incorporated into flight simulation facilities at NASA-Langley, NASA-Ames, and the Lockheed-Georgia Company. When interfaced with advanced air traffic control system models, the facilities will provide full-mission capability for researching issues affecting transport aircraft flight stations and crews of the 1990s.


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    Titel :

    Crew systems and flight station concepts for a 1995 transport aircraft


    Beteiligte:
    Sexton, G. A. (Autor:in)

    Erscheinungsdatum :

    1983-04-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Advanced Concepts Transport Aircraft of 1995

    Sexton, George A. / Chappell, Sheryl L. | SAE Technical Papers | 1985


    Advanced concepts transport aircraft of 1995

    Chappell, S. L. / Sexton, G. A. | NTRS | 1985