Control feel system, adjustable in flight, provided control feel as function of any combination of stick deflection, stick rate, aircraft normal acceleration, pitching acceleration, and pitching velocity; dynamic effects of using varied feel sources in various ratios were measured and/or calculated; frequency response plots illustrate dynamic effects of feel from several sources and combinations thereof.


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    Title :

    Effects of control-feel configuration on airplane longitudinal control response


    Additional title:

    NASA -- Tech Note


    Contributors:
    Crane, H.L. (author) / Sommer, R.W. (author)


    Publication date :

    1961


    Size :

    33 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :





    Longitudinal control feel system for in-flight research on response feel

    Faber, S. / Crane, H.L. | Engineering Index Backfile | 1961