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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    Titel :

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


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Harris, E. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    64 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    System Identification Using Sinusoidal Test Data

    Blakely, Kenneth D. / Dobbs, Michael W. | SAE Technical Papers | 1982



    Flight test of fault-tolerant flight control system using simple adaptive control with PID controller

    Matsuki, Hidenobu / Nishiyama, Taishi / Omori, Yuya et al. | Emerald Group Publishing | 2018