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.
SYSTEME DE COMMANDE POUR COMMANDER AU MOINS UNE HELICE D'UN GIRAVION HYBRIDE, GIRAVION HYBRIDE ET PROCEDE DE COMMANDE ASSOCIE
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
2023-06-21
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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