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. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Approach Path Control for Powered-Lift STOL Aircraft


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

    Erscheinungsdatum :

    1973


    Format / Umfang :

    100 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Approach path control for powered-lift STOL aircraft

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


    Powered lift aerodynamics of USB STOL aircraft

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


    Safety considerations for powered-lift STOL aircraft

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