The results of a piloted simulation experiment to evaluate the effect of integrating flight path angle information into a typical transport electronic attitude director indicator display format for flight director instrument landing system approaches are presented. Three electronic display formats are evaluated during 3 deg straight-in approaches with wind shear and turbulence conditions. Flight path tracking data and pilot subjective comments are analyzed with regard to the pilot's tracking performance and workload for all three display formats.


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    Title :

    Cockpit Simulation Study of Use of Flight Path Angle for Instrument Approaches


    Contributors:
    B. Hanisch (author) / H. Ernst (author) / R. Johnston (author)

    Publication date :

    1981


    Size :

    57 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







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