New design philosophy is that controls and other functional systems, formerly designed separately or by different subcontractors, must be treated as one complete flight control system with aircraft itself to insure acceptable flying conditions over entire mission profile; requirements of automatic systems designed on this basis; consideration of piloted and of automatic loop.


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    Titel :

    Automatic flight control systems requirements for high performance fighter aircraft


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Grossman, N. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1957 Control equipment



    Erscheinungsdatum :

    1957


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Flight Testing of Fighter Aircraft

    A. Knaus / K. H. Burger | NTIS | 1987


    Digital flight control for advanced fighter aircraft

    GRAN, R. / BERMAN, H. / ROSSI, M. et al. | AIAA | 1975