A simulation study was conducted to determine the effectiveness of a simple head-up display in improving glide-slope tracking performance during steep visual approaches in a STOL aircraft. The head-up display featured an attitude-stabilized horizon bar and glide-slope reference bar parallel to and 7.5 deg below the horizon bar. On some approaches a flight-path marker symbol showing the projected ground impact point was also displayed. Half of the approaches were flown in a conventional mode in which the pilot changed pitch attitude to correct for height errors. The remaining approaches were flown in a direct-lift mode in which the pilot modulated thrust to change the flight-path angle without pitching the aircraft.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Head-up displays for STOL visual approaches


    Beteiligte:
    Palmer, E. A. (Autor:in) / Cronn, F. W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.01.1972


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Study of Head-Up Displays for Helicopter/STOL Aircraft

    P. Yiotis / T. Gold / W. Clark | NTIS | 1971



    V/STOL displays for approach and landing

    NATO, Advisory Group for Aerospace Research and Development | TIBKAT | 1972


    VTOL/STOL visual study

    Lewandowski, F. P. | NTRS | 1980


    Vtol/STOL Visual Study

    F. P. Lewandowski | NTIS | 1980