| 摘要 |
The system includes a plurality of engines (m 1 to mn) designed to generate a thrust of the aircraft, each of said engines (m 1 to mn) being controlled by a first controllable actuator (A 1 to An), a plurality of brakes (F 1 to Fm) designed to reduce the speed of the aircraft when it is taxiing, each of said brakes (F 1 to Fm) being controlled by a second controllable actuator (B 1 to Bm), a control unit ( 2 ) designed to generate a piloting setpoint which relates to the longitudinal behavior of the aircraft, and a central processing unit ( 3 A, 3 B) for automatically determining, from the piloting setpoint, a plurality of individual control commands which are applied automatically to the first and second actuators (A 1 to An, B 1 to Bm) and which are used to satisfy the piloting setpoint, and a usage objective for the actuators.
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