An aircraft is provide including an airframe, an extending tail, and a counter rotating, coaxial main rotor assembly including an upper rotor assembly and a lower rotor assembly. A translational thrust system positioned at the extending tail, the translational thrust system providing translational thrust to the airframe. At least one flight control computer configured to independently control the upper rotor assembly and the lower rotor assembly through a fly-by-wire control system. A plurality of sensors to detect sensor data of at least one environmental condition and at least one aircraft state data, wherein the sensors provide the sensor data to the flight control computer.


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    Titel :

    ACTIVE VIBRATION CONTROL OF A ROTORCRAFT


    Weitere Titelangaben:

    AKTIVE SCHWINGUNGSKONTROLLE EINES DREHFLÜGLERS
    CONTRÔLE ACTIF DES VIBRATIONS D'UN GIRAVION


    Beteiligte:

    Erscheinungsdatum :

    16.03.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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