Aircraft piloting method and device for picking up a vertical profile of a flight plan

1. A method of piloting an aircraft to enable the aircraft to pick up and follow a vertical profile of a flight plan, whereby a first piloting mode is used enabling the aircraft to automatically pick up and automatically follow said vertical profile, and a second piloting mode is used enabling the crew of the aircraft to control the picking-up of said vertical profile, the method comprising:

A/ in a first phase:

a) piloting the aircraft according to said second piloting mode enabling the crew of the aircraft to control the picking-up of said vertical profile;

b) determining automatically in real time an engagement zone which is adjacent, by a predetermined value, to an engagement limit zone on the side from which the aircraft arrives at the vertical profile, said engagement limit zone being calculated in real time according to the vertical speed of the aircraft and an angle between a pick-up path and the vertical profile;

c) determining automatically the current position of the aircraft; and

d) automatically comparing this current position to said engagement zone; and

B/ automatically initiating a second phase immediately after said current position of the aircraft is located in said engagement zone, in which the aircraft is piloted according to said first piloting mode which enables the aircraft to automatically pick up and automatically follow said vertical profile, wherein:

within the engagement limit zone, the vertical profile cannot be picked up without overshooting it,

the engagement limit zone is defined about a reference path and surrounds the vertical profile, and

the vertical distance between the upper boundary of the engagement zone and the upper boundary of the engagement limit zone corresponds to a predetermined value.

2. The method as claimed in claim 1 , wherein, in the step A/b), said engagement limit zone is determined in the form of a cylinder.

3. The method as claimed in claim 1 , wherein, in the vertical profile pick-up phase:

the point of intersection between the current path for picking up the vertical profile, followed by the aircraft, and said vertical profile is determined; and

this point of intersection is presented to the crew of the aircraft.

4. The method as claimed in claim 3 , wherein, if said point of intersection does not exist, the crew of the aircraft is notified.

5. The method as claimed in claim 1 , wherein:

said first and second piloting modes are different piloting modes,

said first piloting mode is automatically armed when the crew engages said second piloting mode in the step A/a) in order to control the picking-up of the vertical profile, and

said duly armed first piloting mode is engaged automatically immediately after the current position of the aircraft is located in the engagement zone.

6. The method as claimed in claim 1 , wherein said second piloting mode represents a modified version of said first piloting mode, enabling the crew to control the picking-up of the vertical profile.

7. The method as claimed in claim 1 , wherein said first piloting mode is one of the following modes:

a descent mode, according to which the aircraft is piloted automatically in descent to pick up the vertical profile, then to follow it;

a climb mode, according to which the aircraft is piloted automatically in climbing to pick up the vertical profile, then to follow it.

8. The method as claimed in claim 1 , wherein said second piloting mode is one of the following modes:

a vertical speed mode, enabling the crew to manually control the vertical speed that is applied to the aircraft;

a gradient mode, enabling the crew to manually control the gradient that is applied to the aircraft.

9. A device for piloting an aircraft, which is intended to pilot the aircraft so that it picks up and follows a vertical profile of a flight plan, said device comprising:

a first piloting section that applies a first piloting mode enabling the aircraft to automatically pick up and automatically follow said vertical profile;

a second piloting section that applies a second piloting mode which enables the crew of the aircraft to control the picking-up of said vertical profile;

a first determining section that determines an engagement zone;

a second determining section that determines the current position of the aircraft; and

a comparator that compares this current position to said engagement zone, wherein:

said first determining section automatically determines, in real time, said engagement zone which is adjacent, by a predetermined value, to an engagement limit zone on the side from which the aircraft arrives at the vertical profile, said engagement limit zone being calculated in real time according to the vertical speed of the aircraft and an angle between a pick-up path and the vertical profile; and

said device also comprises a switch that is linked to said first and second piloting sections and which is automatically controlled by said comparator so as to automatically apply to said aircraft:

said second piloting mode applied by said second piloting section in an initial first phase; and

said first piloting mode applied by said first piloting section in a second phase, which begins automatically immediately after said current position of the aircraft is located in said engagement zone, wherein:

within the engagement limit zone, the vertical profile cannot be picked up without overshooting it,

the engagement limit zone is defined about a reference path and surrounds the vertical profile, and

the vertical distance between the upper boundary of the engagement zone and the upper boundary of the engagement limit zone corresponds to a predetermined value.

10. An aircraft, which comprises a device such as that specified under claim 9 .

11. The method of claim 1 , wherein the engagement zone is calculated to account for variations of the vertical speed and an angle between the pick-up path and the vertical profile.