A control system for controlling at least one propeller of a compound rotorcraft, the control system generating a control order for collectively controlling a pitch of the blades of at least one propeller. According to the disclosure, the control system comprises: a first piloting control for generating a first control setpoint; a second piloting control for at least generating a second control setpoint different from first control setpoint; and a control unit configured to generate control order depending on the first control setpoint and second control setpoint, the control unit implementing a control law generating the control order as a function of first control setpoint and the second control setpoint.


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    Title :

    SYSTEME DE COMMANDE POUR COMMANDER AU MOINS UNE HELICE D'UN GIRAVION HYBRIDE, GIRAVION HYBRIDE ET PROCEDE DE COMMANDE ASSOCIE


    Additional title:

    SYSTEM FOR CONTROLLING AT LEAST ONE PROPELLER OF A HYBRID ROTORCRAFT, HYBRID ROTORCRAFT AND ASSOCIATED CONTROL METHOD
    SYSTEM ZUM STEUERN MINDESTENS EINES PROPELLERS EINES HYBRID-DREHFLÜGELFLUGZEUGS, HYBRID-DREHFLÜGELFLUGZEUG UND ENTSPRECHENDES STEUERUNGSVERFAHREN


    Contributors:

    Publication date :

    2023-06-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge