Study conducted by Northrop Corp to determine optimum shaping of control power which provides handling qualities that require little effort on part of pilot to maintain good control; two-axis moving base simulator used and test program for altitude control (throttle), roll, pit and yaw control are described; criterion used to determine optimum control was pilot's opinion based on Cooper rating system; results obtained.


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    Titel :

    Moving base simulator study of all mechanical control system for VTOL aircraft


    Weitere Titelangaben:

    AIAA -- Tech Papers


    Beteiligte:
    Morris, W.B. (Autor:in) / McCormick, R.L. (Autor:in) / Sinacori, J.B. (Autor:in)

    Kongress:

    Simulation for Aerospace Flight Conference ; 1963 VTOL-STOL


    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Moving-base simulator study of an all- mechanical control system for VTOL aircraft

    MCCORMICK, R. / MORRIS, W. / SINACORI, J. | AIAA | 1963


    Moving-base simulator study of an all- mechanical control system for vtol aircraft

    MC CORMICK / R. L. / MORRIS, W. B. et al. | AIAA | 1964


    Simulator investigations of various control systems for VTOL aircraft

    Fry, E. B. / Gerdes, R. M. / Gossett, T. D. et al. | NTRS | 1966


    AUTOLAND SYSTEM FOR VTOL AIRCRAFT, VTOL AIRCRAFT, AND LANDING CONTROL METHOD FOR VTOL AIRCRAFT

    KOJIMA TORU / MORI SATOSHI | Europäisches Patentamt | 2024

    Freier Zugriff

    Flying VTOL Flight Simulator Study

    T. Dukes / R. Gangwish | NTIS | 1960