Longitudinal control on the Lockheed L-1011 is provided by a flying stabilizer. This is the first time such an approach has been used on a United States commercial jet transport.This paper presents the reasons for the choice of longitudinal control systems, and describes the mechanization of the control system with particular emphasis on how it meets Lockheed's safety standards and the Federal Airworthiness Requirements. The status of the ground and flight development tests is discussed.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Development of The Lockheed L-1011's Flying Stabilizer


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    National Air Transportation Meeting ; 1971



    Erscheinungsdatum :

    01.02.1971




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Lockheed L-1011 TriStar

    Kappner, Ulrich | TIBKAT | 1993


    Anschluss verpasst : Lockheed L-1011 Tristar

    Hoeveler, Wolfdietrich | SLUB | 2001


    Flight controls for Lockheed L-1011

    Flapper, J.A. / Throndsen, E.O. | Engineering Index Backfile | 1968