Automatic flight control system (AFCS) for A-7A fighter-attack aircraft is production version of prototype system, developed over 3 yr by Lear Siegler Inc; paper presents developmental philosophy that led to selection of final configuration, completely dual, fixed-gain control-augmentation system, using series hydraulic servos and with attitude, altitude, heading-hold, and heading-select capabilities; results of U S Navy flight evaluation in F-8D aircraft showing capabilities of system in providing improved airplane-handling qualities.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A-7A AFCS -- Flight-proved high-gain system


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Kramer, K.C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    AFCS Integration Requirements

    Chmaruk, B. H. / Lamb, T. R. | SAE Technical Papers | 1981



    A study of (AFCS) communications measurement program

    Breipohl, A.M. / Shanmugam, K.S. / Doemland, H. | Tema Archiv | 1973