| 摘要 |
The inventive device ( 1 ) comprises at least one rudder ( 2 A, 2 B, 2 n), a control unit ( 4 ) for applying a deflexion instruction to the rudder, means ( 6 ) for measuring recovery characteristic displaying the evolution of the aircraft movement in the response to said rudder deflexion instruction, means ( 7 ) for recording at least one applied deflexion instruction and a corresponding recovery characteristic, a servo-control means ( 13 ) for triggering the aircraft in such a way that the recovery characteristic is maintained, wherein the control unit ( 4 ) is provided with means ( 10 ) for receiving an recovery instruction which makes it possible to obtain a recovery characteristic which is identifiable for at least one aerodynamic effect and means ( 11 ) generating the rudder deflexion instruction induced by the recovery instruction.
|
