A rotorcraft control system can include a controller configured to receive an input from a pilot or autopilot for controlling at least one of a rotor and/or a performance profile of the rotorcraft and to control a propulsor as a function of the input for controlling the propulsor relative to the rotor and/or for achieving the input performance profile, wherein the controller is configured to fly the aircraft in accordance with the performance profile or to conform manual control inputs to the performance profile.


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    Titel :

    ROTORCRAFT CONTROL SYSTEMS


    Beteiligte:
    BAZZANI DANIEL (Autor:in) / MACKO NIKOLAS A (Autor:in) / WALTNER PETER J (Autor:in) / WITTMER KENNETH S (Autor:in)

    Erscheinungsdatum :

    18.07.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



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