Concept for development of truly universal automatic flight control system for VTOL aircraft is described; system is built around core system which replaces (typically) mechanical flight control system with "fly-by-wire" controls; principles of inner and outer loop; some of leading problems associated with actual development of such system are indicated; it is believed that achievement of standardized control systems hinges on prior development and acceptance of fly-by-wire control systems.


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    Titel :

    Concept for development of universal automatic flight control system for VTOL aircraft


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Kaufman, L.A. (Autor:in)


    Erscheinungsdatum :

    1965


    Format / Umfang :

    16 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Automatic flight control for VTOL aircraft

    Mueller, L.J. | Engineering Index Backfile | 1966


    Automatic Guidance Concept for VTOL Aircraft

    W. C. HOFFMAN / J. ZVARA / A. E. BRYSON et al. | AIAA | 1971


    An automatic guidance concept for VTOL aircraft

    Bryson, A. E., Jr. / Ham, N. D. / Hoffman, W. C. et al. | NTRS | 1970


    An automatic guidance concept for VTOL aircraft

    BRYSON, JR., A. / HOFFMAN, W. / ZVARA, J. | AIAA | 1970