Method and device for automatically monitoring a flight path of an aircraft during an operation with required navigation performance.

• US 20150073691A1
• Filed: 09/03/2014
• Published: 03/12/2015
• Est. Priority Date: 09/11/2013
• Status: Active Grant

• Current Assignee: Airbus Operations SAS (Airbus SE)
• Original Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Inventors: Mere, Jean-Claude, Tatham, Gilles
• Granted Patent: US 9,368,035 B2
• Time in Patent Office: Days
• US Class Current: 701/120
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0034 Assembly of a flight plan
• CPC Class Codes: G08G 5/0039 Modification of a flight plan

Abstract

A monitoring device including a memory containing a reference path, the memory being separate from a flight management system. The reference path corresponding to a path that is defined during a navigation data validation on ground for the flight management system. A monitoring unit is configured to monitor a current flight path that is determined by the flight management system, by monitoring if this current flight path is in conformity with the reference flight path that is recorded in the memory.

Claims

1. A method for automatically monitoring a flight path of an aircraft during at least one required navigation performance operation, comprising the steps:

determining said flight path, which is intended for the required navigation performance operation, by a flight management system of the aircraft using navigation data stored in a database on board the aircraft,

determining, on the ground, during a validation of the navigation data intended to be stored in said on-board database, a path using a simulator which simulates the functioning of the aircraft, and to which said navigation data are applied, the path thus determined being considered to be the reference path,

said method also comprising the following steps a) and b), taking place on the aircraft, of;

a) logging the reference path in a memory on board the aircraft, said memory being independent of a sequence for calculating the flight path comprising at least said flight management system, the reference path representing the path defined in the previous step during the ground validation of said navigation data; and

b) using said reference path to monitor a current flight path determined by the flight management system by verifying the consistency between said current flight path and said reference path.

2. The method according to claim 1, comprising an additional step, after step b), comprising:

presenting monitoring results to the crew, at least in the event of inconsistency between the current flight path determined by the flight management system and the reference path.

3. The method according to claim 1, wherein, in step a), in addition to the reference path, procedural information is also logged in the on-board memory.

4. The method according to claim 1, wherein, in step a), logging in the on-board memory is carried out in a coded manner.

5. The method according to claim 1, wherein, in step b), said current flight path is compared with said reference path, and it is considered to be consistent if it does not depart therefrom by a first predefined close margin.

6. The method according to claim 1, comprising, in addition, steps comprising:

logging flight paths of the aircraft determined by a position calculation unit during required navigation performance operations; and

calculating an average path using said flight paths thus logged.

7. The method according to claim 6, wherein, in step b), said current flight path is compared with said average path, and it is considered to be consistent if it does not depart therefrom by a second predefined close margin.

8. The method according to claim 6, comprising steps comprising:

calculating the difference between said average path and said reference path so as to obtain a bias;

adding this bias to a current flight path determined by said flight management system so as to form a corrected current path; and

comparing, in step b), this corrected current path with said reference path in order to verify the consistency.

9. The method according to claim 1, comprising additional steps, after step b), comprising, in real-time, during the implementation of a required navigation performance operation:

determining the current position of the aircraft; and

comparing this current position with the current flight path determined by the flight management system for said required navigation performance operation.

10. A device for automatically monitoring a flight path of an aircraft during at least one required navigation performance operation, said flight path which is intended for a required navigation performance operation being determined by a flight management system of the aircraft using navigation data stored in a database on board the aircraft, said device comprising:

an on-board memory in which a reference path is stored, said memory being independent of a sequence for calculating the flight path comprising at least said flight management system, said reference path representing a path defined on the ground, during a validation of the navigation data intended to be stored in said on-board database using a simulator which simulates the functioning of the aircraft, and to which said navigation data are applied; and

a monitoring unit configured to monitor a current flight path determined by the flight management system by verifying the consistency between said current flight path and the reference path logged in said on-board memory.

11. The device according to claim 10, further comprising:

a logging unit configured to log, in an auxiliary memory, flight paths of the aircraft determined by a position calculation unit during required navigation performance operations; and

a first calculation unit configured to calculate an average path using said flight paths logged in said auxiliary memory.

12. The device according to claim 11, further comprising:

a second calculation unit configured to calculate the difference between said average path and said reference path so as to obtain a bias;

a third calculation unit configured to add this bias to a current flight path determined by said flight management system so as to form a corrected current path; and

a first comparison element configured to compare this corrected current path with said reference path to verify the consistency.

13. The device according to claim 10, further comprising:

a position calculation unit configured to determine, in real-time, the current position of the aircraft during the implementation of a required navigation performance operation; and

a second comparison element configured to compare, in real-time, this current position with the current flight path determined by the flight management system.

14. An aircraft, comprising a device for automatically monitoring a flight path of an aircraft during at least one required navigation performance operation, said flight path which is intended for a required navigation performance operation being determined by a flight management system of the aircraft using navigation data stored in a database on board the aircraft, said device comprising:

an on-board memory in which a reference path is stored, said memory being independent of a sequence for calculating the flight path comprising at least said flight management system, said reference path representing a path defined on the ground, during a validation of the navigation data intended to be stored in said on-board database using a simulator which simulates the functioning of the aircraft, and to which said navigation data are applied; and

a monitoring unit configured to monitor a current flight path determined by the flight management system by verifying the consistency between said current flight path and the reference path logged in said on-board memory.