Development and evaluation in flight of adjustable system; variable feel was provided from stick position, stick rate, normal acceleration, pitching acceleration, and pitching velocity; operation was satisfactory and illustrated effects of large amounts of response feel on stability of controlfree aircraft and control system response.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    NASA -- Tech Note


    Contributors:
    Faber, S. (author) / Crane, H.L. (author)


    Publication date :

    1961


    Size :

    31 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




    Effects of control-feel configuration on airplane longitudinal control response

    Crane, H.L. / Sommer, R.W. | Engineering Index Backfile | 1961