Study of system suitable for high performance aircraft and missiles measuring vehicle response to small amplitude control surface deflections produced by sinusoidal test signal; changes in response to signal are related to environmental changes; system is continuously altered to maintain response equal to preselected value; effects on system performance of variation in flight condition, system gain level, test signal frequency, and sensor location.


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    Title :

    Analytical investigation of adaptive flight-control system using sinusoidal test signal J


    Additional title:

    NASA -- Tech Note


    Contributors:
    Harris, E. (author)


    Publication date :

    1961


    Size :

    64 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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