| 摘要 |
The piloting device (1) comprises means (2A, 2B) for generating orders for the control of control surfaces (3A, 3B, 3C, 3D) capable of acting on the yaw movement of the aircraft and each controlled by at least one actuator (4A, 4B, 4C, 4D), and a central unit (UC) which comprises means (5A, 5B) for determining an instruction to rotate the aircraft, based on control orders, means (6) for determining a global moment having to be applied to the aircraft about the yaw axis so that the aircraft performs the rotation instruction, means (7) for dividing this global moment into a sum of elementary moments, and means (7) for computing, for each of the control surfaces (3A, 3B, 3C, 3D), the instruction to be applied to its actuator (4A, 4B, 4C, 4D) so that the latter generates the associated elementary moment.
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