The flight profile indicator (FPI) was evaluated in a treatment by subject analysis of variance experimental design using six helicopter-rated subjects. A 15-degree and a 5-degree instrument approach were flown with and without the FPI, using a simulation of the Norden-developed integrated electronic vertical display (IEVD), vertical speed indicator, and bearing, distance, heading indicator as an instrument panel, and a simulation of the UH-1 as the vehicle using the Honeywell hybrid computer facility. Each subject flew 20 five-minute training flights, and 40 five-minute data gathering flights, 10 per condition. Data from 10 dependent variables, objective and subjective, were gathered. (Author)


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    Titel :

    Simulator Evaluation of the Flight Profile Indicator


    Beteiligte:
    M. W. Gaynor (Autor:in)

    Erscheinungsdatum :

    1970


    Format / Umfang :

    53 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    The Design of an EFIS Attitude Indicator for a Flight Simulator

    Handley, S. J. / Allerton, D. J. | British Library Online Contents | 1994


    The Design of an EFIS Attitude Indicator for a Flight Simulator

    Handley, S. J. / Allerton, D. J. / International Council of Aeronautical Sciences | British Library Conference Proceedings | 1994