An in-flight simulation was undertaken to study the piloting problems associated with a type of nonlinear control effectiveness which is characteristic of spoiler roll control systems. Typically, the initial response is small or even zero, followed by a narrow region of highly effective control, and a final one of moderate effectiveness.Results for the landing flare and touchdown, which turned out to be the critical flight phase, indicate that a substantial amount of dead zone and changing effectiveness can be tolerated, but the best level of handling is obtained with linear, aileron-like control.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    An In-Flight Investigation of Nonlinear Roll Control


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    National Business Aircraft Meeting and Engineering Display ; 1975



    Erscheinungsdatum :

    1975-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    An in-flight investigation of nonlinear roll control

    Ellis, D. R. / Tilak, N. W. | NTRS | 1975



    NONLINEAR FLIGHT PHYSICS OF THE LIE-BRACKET ROLL MECHANISM

    Taha, Haitham E. / Hassan, Ahmed | TIBKAT | 2021


    Nonlinear Flight Physics of the Lie-Bracket Roll Mechanism

    Taha, Haitham E. / Hassan, Ahmed | AIAA | 2021