A rotorcraft autopilot system includes a series actuator connecting a cockpit control component to a swashplate of a rotorcraft, the series actuator to modify a control input from the cockpit control component to the swashplate through a downstream control component. The rotorcraft autopilot system also includes a differential friction system connected to the cockpit control component, the differential friction system to control the series actuator to automatically adjust a position of the cockpit control component during rotorcraft flight based, in part, on a flight mode of the rotorcraft.


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    Titel :

    Rotorcraft autopilot control


    Beteiligte:
    GRIFFITH CARL D (Autor:in) / ATKINS BRADY G (Autor:in) / RAZA AWAIS (Autor:in) / WILSON PAUL M (Autor:in)

    Erscheinungsdatum :

    16.01.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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