Active controls in the Lockheed L-1011 for increased energy efficiency are discussed. Active wing load alleviation for extended span, increased aspect ratio, and active stability augmentation with a smaller tail for reduced drag and weight are among the topics considered. Flight tests of active wing load alleviation on the baseline aircraft and moving-base piloted simulation developing criteria for stability augmentation are described.


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    Titel :

    Development and flight evaluation of active controls in the L-1011


    Beteiligte:
    Johnston, J. F. (Autor:in) / Urie, D. M. (Autor:in)


    Erscheinungsdatum :

    01.01.1978


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Flight controls for Lockheed L-1011

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


    L-1011 flight test program

    WOODMAN, J. | AIAA | 1971




    Nr. 1011

    DataCite | 1864

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