An aircraft includes an airframe having an extending tail, a counter rotating, coaxial main rotor assembly disposed at the airframe including an upper rotor assembly and a lower rotor assembly, and a translational thrust system positioned at the extending tail and providing translational thrust to the airframe. A fly by wire control system for the aircraft includes a flight control system configured to receive a plurality of inputs and a flight control computer to translate the inputs into commands and issue the commands to one or more controlled elements of the aircraft. A fly by wire control system for a dual coaxial rotor rotorcraft with auxiliary propulsor includes a flight control system configured to receive a plurality of inputs and a flight control computer to translate the inputs into commands and issue the commands to one or more controlled elements of the rotorcraft.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ROTORCRAFT SYSTEMS TO REDUCE PILOT WORKLOAD


    Beteiligte:
    BREDENBECK KEVIN L (Autor:in) / WEINER STEVEN D (Autor:in) / WALSH DAVID M (Autor:in) / COTTON BRYAN S (Autor:in) / ARIFIAN KENNETH C (Autor:in)

    Erscheinungsdatum :

    2017-10-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Inflight evaluation of pilot workload measures for rotorcraft research

    Shively, Robert J. / Bortolussi, Michael R. / Battiste, Vernol et al. | NTRS | 1987


    Does the 'silent cockpit' reduce pilot workload?

    Hoogeboom, P. / Joosse, M. / Hodgetts, H. et al. | IEEE | 2004


    Does The `Silent Cockpit' Reduce Pilot Workload?

    Hoogeboom, P. / IEEE / AIAA | British Library Conference Proceedings | 2004