Study of closed loop rate feedback system to determine applicability to high speed, high altitude aircraft; advantages are fully maneuverable aircraft, minimum of programming to obtain desired flying characteristics, reduction of weight over mechanical system, and flexibility previously unobtainable; study of possible ways to improve reliability of control system electronic equipment.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Analysis of electrical flight-control system for interceptor-type aircraft


    Weitere Titelangaben:

    Aeronautical Eng Rev


    Beteiligte:
    Price, E. (Autor:in) / Westerwick, R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1957


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





    Interim interceptor: analysis

    Anderton, D.A. | Engineering Index Backfile | 1953


    Sabot high speed interceptor AE 4273 aircraft design

    Dober, Dave / Al-Hashel, Waleed / Baldocchi, Bob et al. | NTRS | 1992