The use of control system design to enhance high-angle-of-attack flying qualities and departure/spin resistance has become an accepted and widely used approach for modern fighter aircraft. NASA and the Navy are currently conducting a joint research program to investigate the application of this technology to the F-14. The paper discusses the results of this program within the context of its contributions to advancing high-alpha control system technology. General topics covered include (1) analysis and design tools, (2) control system design approach, and (3) flight test approach and results.


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    Titel :

    Application of high-alpha control system concepts to a variable-sweep fighter airplane


    Beteiligte:
    Nguyen, L. T. (Autor:in) / Gilbert, W. P. (Autor:in) / Gera, J. (Autor:in) / Iliff, K. W. (Autor:in) / Enevoldson, E. K. (Autor:in)

    Kongress:

    Atmospheric Flight Mechanics Conference ; 1980 ; Danvers, MA


    Erscheinungsdatum :

    1980-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch