A study was conducted to explore the feasibility of a safety margin system for powered-lift aircraft which require a backside piloting technique. The objective of the safety margin system was to present multiple safety margin criteria as a single variable which could be tracked manually or automatically and which could be monitored for the purpose of deriving safety margin status. The study involved a pilot-in-the-loop analysis of several safety margin system concepts and a simulation experiment to evaluate those concepts which showed promise of providing a good solution. A system was ultimately configured which offered reasonable compromises in controllability, status information content, and the ability to regulate the safety margin at some expense of the allowable low speed flight path envelope.


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    Titel :

    Study of a safety margin system for powered-lift STOL aircraft


    Beteiligte:
    Heffley, R. K. (Autor:in) / Jewell, W. F. (Autor:in)

    Erscheinungsdatum :

    1978-05-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Safety considerations for powered-lift STOL aircraft

    Holzhauser, C. A. / Innis, R. C. | NTRS | 1971


    Powered lift aerodynamics of USB STOL aircraft

    MAITA, M. / FUJIEDA, H. / MORITA, M. et al. | AIAA | 1983


    Operational experience with a powered-lift STOL aircraft

    Innis, R. C. / Quigley, H. C. | NTRS | 1976


    Ground Effects on Lift for Turbofan Powered-Lift STOL Aircraft

    John P. Campbell / James L. Hassel James L. Thomas | AIAA | 1978


    Approach path control for powered-lift STOL aircraft

    Clymer, D. J. / Flora, C. C. | NTRS | 1973