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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    Aeronautical Eng Rev


    Contributors:
    Price, E. (author) / Westerwick, R. (author)

    Published in:

    Publication date :

    1957


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :





    Interim interceptor: analysis

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


    Extended Range Interceptor (ERINT-1) flight test program

    WALTERS, EDWARD / BUTLER, JOSEPH | AIAA | 1992