Method and device for providing an aircraft with a flight trajectory

• US 7,349,773 B2
• Filed: 05/02/2005
• Issued: 03/25/2008
• Est. Priority Date: 05/18/2004
• Status: Active Grant

• Current Assignee: Airbus Operations SAS (Airbus SE)
• Original Assignee: Airbus France
• Inventors: Berard, Jérémy
• Primary Examiner(s): Camby; Richard M.
• Application Number:
  US11/118,315
• Publication Number:
  US 20060085101A1
• Time in Patent Office: 1,058 Days
• Field of Search: 701/3, 701/4, 701/11, 701/200, 701/201, 701/207, 701/208, 701/209, 701/210, 701/224, 342/357.13, 342/357
• US Class Current: 701/3
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G05D 1/0202 specially adapted to aircraft

Abstract

A device includes a first unit for defining a main trajectory, which is followed by the aircraft, and an optional trajectory which deviates from the main trajectory, which exhibits at least one common point shared with said main trajectory and which is able to be followed by the aircraft if the trajectory is activated. The device also includes a second unit for automatically determining a decision point which indicates the last position of the aircraft along the main trajectory, where the optional trajectory can still be activated so as to allow the aircraft to follow it. The device further includes a third unit for automatically presenting the decision point to a pilot of the aircraft, and an actuatable unit which allows a pilot to activate the optional trajectory.

Claims

1. A method for providing an aircraft with a flight trajectory, said method comprising:

a) defining a main trajectory (TP), which is followed by the aircraft, and at least one optional trajectory (TO) which deviates from said main trajectory (TP), which exhibits at least one common point (TC) shared with said main trajectory (TP) and which is able to be followed by the aircraft if said trajectory is activated;

b) determining automatically a decision point (5) which indicates the last position of the aircraft along said main trajectory (TP), where said optional trajectory (TO) can still be activated so as to allow the aircraft to follow it;

c) presenting automatically said decision point (5) to a pilot of the aircraft; and

d) the pilot can, at least as a function of this presentation, activate said optional trajectory (TO).

2. The method as claimed in claim 1,

wherein, to determine said decision point (5):

on the basis of said common point, successively, for each point following said main trajectory (TP), in the direction of flight of the aircraft , a check is carried out to verify whether this point also belongs to said optional trajectory (TO); and

as soon as a point no longer belongs to said optional trajectory (TO), account is taken of the previous point which still belonged to said optional trajectory (TO) and this previous point is regarded as decision point (5).

3. The method as claimed in claim 2,

wherein a check is carried out to verify, in a lateral plane, whether a point of the main trajectory (TP) also belongs to the optional trajectory (TO).

4. The method as claimed in claim 2,

wherein a check is carried out to verify, in the whole of space, whether a point of the main trajectory (TP) also belongs to the optional trajectory (TO).

5. The method as claimed in claim 1,

wherein, if in step d) the pilot activates said optional trajectory (TO) which then becomes the new trajectory followed by the aircraft, the main trajectory (TP) initially followed by the aircraft is transformed into a new optional trajectory.

13. An aircraft,

which comprises a device capable of implementing the method specified under claim 1.

6. A device for providing an aircraft, with a flight trajectory,

which device comprises:

first means for defining a main trajectory (TP), which is followed by the aircraft, and an optional trajectory (TO) which deviates from said main trajectory (TP), which exhibits at least one common point (TC) shared with said main trajectory (TP) and which is able to be followed by the aircraft if said trajectory is activated;

second means for automatically determining a decision point (5) which indicates the last position of the aircraft along said main trajectory (TO), where said optional trajectory (TO) can still be activated so as to allow the aircraft to follow it;

third means for automatically presenting said decision point (5) to a pilot of the aircraft; and

fourth means which are actuatable, allowing a pilot to activate said optional trajectory (TO).

7. The device as claimed in claim 6,

wherein said third means comprise a head-up display screen (8).

8. The device as claimed in claim 6,

wherein said third means comprise a head-down display screen.

9. The device as claimed in claim 6,

wherein said fourth means comprise interactive means of control.

10. An automatic guidance system for an aircraft, said guidance system (SG) comprising:

a set of information sources;

an auxiliary source of information able to provide a flight trajectory;

a central unit for automatically determining orders for steering the aircraft, with the aid of information received from said set of information sources and a flight trajectory (TP, TO) provided by said auxiliary source of information; and

means of actuation of controlled members of the aircraft, to which the steering orders determined by said central unit are applied automatically,

wherein said central auxiliary source of information comprises a device such as specified under claim 6, for providing a flight trajectory (TP, TO).

11. An aircraft,

which comprises a guidance system (SG) such as that specified under claim 10.

12. An aircraft,

which comprises a device such as that specified under claim 6.