A method of controlling a helicopter having a rotor with blades is provided. The method includes receiving, by a computing device comprising a processor, at least one input associated with the helicopter; generating, by the computing device, control signals configured to counteract blade bending associated with the rotors based on the received at least one input; measuring, by the computing device, blade signals using sensors for the blades; extracting, by the computing device, harmonic loads from the measured blade signals; adapting, by the computing device, the control signals based on the harmonic loads; and controlling, by the computing device, servos connected to the blades to adjust the blades according to the adapted control signals to reduce vibratory loads on the blades.


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    Titel :

    HELICOPTER ROTOR LOAD REDUCTION AND TIP CLEARANCE CONTROL


    Weitere Titelangaben:

    HUBSCHRAUBERROTOR-LASTVERRINGERUNG UND SPITZENSPIELRAUMSTEUERUNG
    RÉDUCTION DE LA CHARGE D'UN ROTOR D'HÉLICOPTÈRE ET COMMANDE DE DÉBATTEMENT EN BOUT DES PALES


    Beteiligte:
    ELLER EREZ (Autor:in) / KNAG JOHN (Autor:in)

    Erscheinungsdatum :

    11.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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