OPTIMIZATION OF THE TRAJECTORY OF AN AIRCRAFT

• US 20150323933A1
• Filed: 05/08/2015
• Published: 11/12/2015
• Est. Priority Date: 05/09/2014
• Status: Abandoned Application

• Current Assignee: Thales SA
• Original Assignee: Thales SA
• Inventors: LE MERRER, Mathieu, BOYER, Johan, DARBOIS, Alexandre
• Application Number:
  US14/707,946
• Publication Number:
  US 20150323933A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G05D 1/0005 with arrangements to save energy
• CPC Class Codes: G05D 1/0202 specially adapted to aircraft

Abstract

A method implemented by computer for optimizing the cruising trajectory of an aircraft comprises the steps consisting in receiving the parameters of a reference trajectory, the trajectory comprising one or more plateaus and the transitions between these plateaus, the transitions being ascending or descending; and determining, in response to a request received in the course of the flight, at least one candidate alternative trajectory; and determining one or more indicators associated with the candidate alternative trajectory such as determined. Developments comprise the optional display of at least one indicator, indicators associated with the fuel consumption, with a difference in flight time or with the operational cost of the flight of the aircraft, the use of ratios of indicators, the inhibition of descending transitions, particular plateau length transitions as well as economical modes of transition. System aspects are described, comprising avionic or non-avionic means.

Claims

1. A method implemented by computer for optimizing the cruising trajectory of an aircraft comprising the steps:

receiving the parameters of a reference trajectory, the said trajectory comprising one or more plateaus and the transitions between the said plateaus, the said transitions being ascending or descending;

determining, in response to a request received in the course of the flight, at least one candidate alternative trajectory; and

determining one or more indicators associated with the candidate alternative trajectory such as determined;

said determining a candidate alternative trajectory comprising a step consisting in inhibiting the descending transitions.

2. The method according to claim 1, further comprising displaying at least one indicator.

3. The method according to claim 1, an indicator being associated with the fuel consumption of the aircraft.

4. The method according to claim 1, an indicator being associated with the flight time of the aircraft.

5. The method according to claim 1, an indicator being associated with the operational cost of the flight of the aircraft.

6. The method according to claim 1, further comprising receiving the selection of a ratio of one or more indicators.

7. The method according to claim 1, said determining a candidate alternative trajectory comprising a step consisting in favouring a transition to a plateau if the length associated with the said plateau is longer than a predefined threshold.

8. The method according to claim 1, further comprising receiving an indication of selection of a candidate alternative trajectory.

9. The method according to claim 8, further comprising realization by the aeroplane of the selected candidate alternative trajectory.

10. The method according to claim 9, further comprising realization of a transition between plateaus of the selected trajectory, the said transition being performed according to a predefined mode.

11. A computer program product, comprising code instructions making it possible to perform the steps of the method according to claim 1, when the said program is executed on a computer.

12. A system comprising means for implementing one or more steps of the method according to claim 1.

14. The system according to claim 12, comprising non-avionic means of electronic flight bag type.

13. The system according to claim 13, comprising avionic means of FMS flight management system type.