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.


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    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 :





    Extended Range Interceptor (ERINT-1) flight test program

    WALTERS, EDWARD / BUTLER, JOSEPH | AIAA | 1992


    Interceptor vehicles

    Johnson, A.F. | Engineering Index Backfile | 1960