A flight control system concept is defined for approach flightpath control of an augmentor wing (or similar) powered-lift STOL configuration. The proposed STOL control concept produces aircraft transient and steady-state control responses that are familiar to pilots of conventional jet transports, and has potential for good handling qualities ratings in all approach and landing phases. The effects of trailing-edge rate limits, real-engine dynamics, and atmospheric turbulence are considered in the study. A general discussion of STOL handling qualities problems and piloting techniques is included.


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    Titel :

    Approach path control for powered-lift STOL aircraft


    Beteiligte:
    Clymer, D. J. (Autor:in) / Flora, C. C. (Autor:in)

    Erscheinungsdatum :

    1973-04-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Approach Path Control for Powered-Lift STOL Aircraft

    D. J. Clymer / C. C. Flora | NTIS | 1973


    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


    Flight Reference Display for Powered-Lift STOL Aircraft

    K. Tanaka / K. Funabiki / M. Nakamura et al. | NTIS | 1994


    Ground Effects on Lift for Turbofan Powered-Lift STOL Aircraft

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