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.
CONTROL SYSTEM FOR CONTROLLING AT LEAST ONE PROPELLER OF A COMPOUND ROTORCRAFT, ASSOCIATED COMPOUND ROTORCRAFT AND CONTROL METHOD
2022-09-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |