| 摘要 |
<p>Aircraft command and control unit, in particular for flight control surfaces of an aircraft, and for controlling and commanding aircraft devices that require aerodynamic control, comprising: -actuating means for moving flight control surfaces; an automatic flight control system for the aircraft or aircraft device, connected to the actuating means for moving the flight control surfaces; and -at least one flight controller (1) on which the operator or pilot acts, and that receives a force (2) applied by the pilot, connected to the automatic flight control system and to the actuating means for moving the flight control surfaces, and that comprises: -means to generate force on the controller and -means to detect the position of the controller; the flight controller (1) also comprising: -means to detect the force (2) applied to the controller (1); and at least one control unit that receives information on the position of the controller (1) and the force (2) applied to the controller, sending this information to the means of generating force on the controller (1).</p> |
