A method of controlling at least a first pitch of a first propeller and a second pitch of a second propeller of a hybrid helicopter, the hybrid helicopter having a thrust control and a yaw control that are configured to generate orders for modifying respectively a mean pitch component and a differential pitch component of the first pitch and of the second pitch, the hybrid helicopter having a collective pitch control for modifying a collective pitch component of main blades of the lift rotor. The method includes a step of: keeping with the control system the first pitch and the second pitch within a control domain that varies as a function of information relating to the collective pitch component.
METHOD OF CONTROLLING PROPELLERS OF A HYBRID HELICOPTER, AND A HYBRID HELICOPTER
2021-09-23
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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