| 主权项 |
1. An aircraft flight control method, the comprising:
a) a step of generating a load factor control value, this load factor control value being representative of manual actuation of a control column of the aircraft by a pilot of the aircraft; b) a step of calculating at least one deflection instruction of at least one elevator of the aircraft from the load factor control value; and c) a step of applying at least one calculated deflection instruction to the elevator so as to modify the angle of attack of the aircraft and its lift, in which method: step b) comprises: b1) dividing the load factor control value into a first value and a second value; b2) using the first value, calculating a deflection instruction of the elevator; and b3) using the second value, calculating at least one command instruction of at least one lift generator element of the aircraft, said lift generator element being able to modify directly the lift of the aircraft; and step c) comprises sub-steps consisting in: c1) applying said deflection instruction to said elevator; and c2) applying said command instruction to said at least one lift generator element, said first and second values being defined so that, when the corresponding deflection instruction and the corresponding command instruction are definitively applied to the elevator and to the at least one lift generator element, respectively, the latter generate the same aerodynamic position of the aircraft as if a deflection instruction determined from the whole of the load factor control value were applied only to the elevator. |
