Device, system and method of estimating the angle of attack of an aircraft

1. A device for estimating an estimated fuselage angle of attack of an aircraft moving in the air, the device comprising:

a sensor that measures an attack angle based on a direction of the air flowing relative to at least one point on a surface of the aircraft;

a memory that stores correspondence tables, each correspondence table is associated with a different configuration of positions of lift devices of the aircraft, and each correspondence table includes entries that relate the measured attack angle and a speed information item about an airspeed of the aircraft to a corresponding estimated fuselage angle of attack of the fuselage of the aircraft; and

a determining section that selects a correspondence table stored in the memory that is associated with the current position of the lift devices of the aircraft, and selects an entry in the selected correspondence table based on the measured attack angle and the speed information item about the airspeed of the aircraft as the estimated fuselage attack angle of the aircraft.

2. The device according to claim 1 , comprising a selecting section that selects the correspondence table as a function of a lift device information item indicative of the configuration of the lift devices of the aircraft.

3. The device according to claim 1 , wherein the speed information item is a Mach number of the aircraft.

4. The device according to claim 1 , comprising a speed determining section that determines the speed information item as a function of a static pressure information item and of a total pressure information item.

5. A system for estimating an estimated fuselage angle of attack of an aircraft moving in the air, the system comprising:

a sensor configured to measure a measured attack angle based on a direction of the air flowing relative to at least one point on a surface of the aircraft;

a module that receives the measured fuselage attack angle from the sensor;

a memory that stores correspondence tables, each correspondence table is associated with a different configuration of positions of lift devices of the aircraft, and each correspondence table includes entries that relate the measured attack angle and a speed information item about an airspeed of the aircraft to a corresponding estimated fuselage angle of attack of the fuselage of the aircraft; and

a determining section that selects a correspondence table stored in the memory that is associated with the current position of the lift devices of the aircraft, and selects an entry in the selected correspondence table based on the measured attack angle and the speed information item about the airspeed of the aircraft as the estimated fuselage attack angle of the aircraft.

6. The system according to claim 5 , wherein the sensor includes a vane mounted on a pivot in such a way as to become positioned parallel to the air stream.

7. A method for estimating an estimated fuselage angle of attack of an aircraft moving in the air, the method comprising:

measuring, using a sensor, a measured fuselage attack angle based on a direction of the air flowing relative to at least one point on a surface of the aircraft;

storing plural correspondence tables each associated with a different configuration representative of positions of lift devices of the aircraft, each correspondence table including entries that relate the measured fuselage attack angle and a speed information item about an airspeed of the aircraft to the estimated fuselage angle of attack of the fuselage of the aircraft; and

selecting a stored correspondence table that is associated with the current position of the lift devices of the aircraft, and select an entry in the selected correspondence table based on the measured attack angle and the speed information item about the airspeed of the aircraft as the estimated fuselage attack angle of the aircraft.

8. The method according to claim 7 , further comprising selecting the correspondence table as a function of a lift device information item indicative of the configuration of the lift devices of the aircraft.

9. The method according to claim 7 , wherein the speed information item is a Mach number of the aircraft.

10. The method according to claim 7 , wherein the measuring includes positioning, parallel to the air stream, a pivot-mounted vane.