To establish handling quality requirements for VTOL and STOL aircraft, need exists for simulator which reproduces dynamic responses of vehicle; variable stability helicopter was constructed in such way to vary stability and control parameters requiring investigation by making suitable adjustments to electrical analog models inserted between pilot's controls and autopilot system; installation and tests of autopilot, analog computer, and other equipment installed in H-13G helicopter are described; flight test data.


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    Titel :

    Development of model-controlled V/STOL airborne simulator


    Weitere Titelangaben:

    Canada. Nat Research Council -- Aeronautical Report


    Beteiligte:
    Daw, D. (Autor:in) / McGregor, D.M. (Autor:in)


    Erscheinungsdatum :

    1962


    Format / Umfang :

    90 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The NAE airborne V/stol simulator

    Sinclair, S.R.M. / Roderick, W.E.B. / Lum, K. | Tema Archiv | 1977


    Description of four degrees of freedom, V/STOL aircraft, airborne simulator

    Daw, D.F. / Lum, K. / McGregor, D.M. | Engineering Index Backfile | 1968