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    Computer Simulation of Multiple Pilots Flying a Modern High Performance Helicopter

    Computer Simulation of Multiple Pilots Flying a Modern High Performance Helicopter


    A computer simulation of a human response pilot mechanism within the flight control loop of a high-performance modern helicopter is presented. A human response mechanism, implemented by a low order, linear transfer function, is used in a decoupled single variable configuration that exploits the dominant vehicle characteristics by associating cockpit controls and instrumentation with specific vehicle dynamics. Low order helicopter models obtained from evaluations of the time and frequency domain responses of a nonlinear simulation model, provided by NASA Lewis Research Center, are presented and considered in the discussion of the pilot development. Pilot responses and reactions to test maneuvers are presented and discussed. Higher level implementation, using the pilot mechanisms, are discussed and considered for their use in a comprehensive control structure.

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    Titel :

    Computer Simulation of Multiple Pilots Flying a Modern High Performance Helicopter

    Beteiligte:
    M. E. Zipf (Autor:in) / W. G. Vogt (Autor:in) / M. H. Mickle (Autor:in) / R. G. Hoelzeman (Autor:in) / F. Kai (Autor:in)
    Erscheinungsdatum :

    1988

    Format / Umfang :

    32 pages

    Medientyp :

    Report

    Format :

    Keine Angabe

    Sprache :

    Englisch

    Schlagwörter :

    Aircraft , Test Facilities & Equipment , Computerized simulation , Helicopters , Control systems design , Human factors engineering , Pilot performance , Cockpits , Dynamic control , Feedback control , Flight control , Nonlinear systems , Transfer functions

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