The primary objective of the study was to investigate, by means of real-time man-in-the-loop simulation techniques, piloting performance as influenced by wind, system data-rate, and contingency-event variables during IFR steep approaches with vertical-lift aircraft. By also simultaneously evaluating effects of display-format, approach-angle and measurement-noise variables to the extent possible within the scope of each study task, an increased degree of generality of study results was obtained. A variable-velocity simulation of the Bell UH-i helicopter served as the test vehicle in all study tasks. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    IRF Steep-Angle Approach: Effects of Wind, System Data-Rate, and Contingency-Event Variables


    Beteiligte:
    J. D. Wolf (Autor:in) / M. F. Barrett (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    262 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Aircraft Displays for Steep-Angle Approaches

    J. D. Wolf / R. B. Hoppe | NTIS | 1970


    Steep steep detection

    WALKER BRUCE M / BOOTE JOHN | Europäisches Patentamt | 2023

    Freier Zugriff

    Steep-angle conveying installation for open-cast mining

    BECKER HANS-JÜRGEN / WERRE KLAUS | Europäisches Patentamt | 2018

    Freier Zugriff