GB2635621A - A system and method for optimising flight efficiency - Google Patents
A system and method for optimising flight efficiency Download PDFInfo
- Publication number
- GB2635621A GB2635621A GB2500657.8A GB202500657A GB2635621A GB 2635621 A GB2635621 A GB 2635621A GB 202500657 A GB202500657 A GB 202500657A GB 2635621 A GB2635621 A GB 2635621A
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- flight
- aircraft
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/20—Arrangements for acquiring, generating, sharing or displaying traffic information
- G08G5/21—Arrangements for acquiring, generating, sharing or displaying traffic information located onboard the aircraft
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/30—Flight plan management
- G08G5/32—Flight plan management for flight plan preparation
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/50—Navigation or guidance aids
- G08G5/54—Navigation or guidance aids for approach or landing
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/50—Navigation or guidance aids
- G08G5/55—Navigation or guidance aids for a single aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/70—Arrangements for monitoring traffic-related situations or conditions
- G08G5/76—Arrangements for monitoring traffic-related situations or conditions for monitoring atmospheric conditions
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Feedback Control In General (AREA)
Abstract
A method and system for improving the fuel efficiency of an aircraft flight, and a method for training a machine learning module to predict the most probable descent flight trajectories are disclosed. The machine learning module uses two stages of clustering and regression analysis to analyse historical flight data, so that the trained model can determine the most probable flight trajectory for the descent phase of a future / ongoing flight. This can then be used to determine an adjusted top of descent and output to the pilot of the future / ongoing flight, or used to control an associated autopilot system.
Claims (21)
1 . A method for improving the fuel efficiency of an aircraft flight, the method comprising: storing, in a flight plan data store, a flight plan for the aircraft flight, the flight plan comprising a scheduled route for the aircraft flight, a scheduled landing runway at a destination aerodrome, and a scheduled arrival time and date at the destination aerodrome; storing, in a weather data store, predicted weather data corresponding to the vicinity of the airport at the scheduled arrival time and date; receiving, at a first cluster mapping module of a trained machine learning prediction module, the scheduled route for the aircraft flight, the scheduled landing runway at a destination aerodrome, and the predicted weather data corresponding to the vicinity of the destination aerodrome at the scheduled arrival time and date; determining, by the first cluster mapping module, based on the trained machine learning of the prediction module, a predicted arrival route and a predicted landing runway; determining, by a second cluster mapping module of the trained machine learning prediction module, based on the predicted arrival route and the predicted landing runway, a plurality of descent flight trajectories for the aircraft flight; filtering, by a trajectory filter of the trained machine learning prediction module, to obtain the most probable descent flight trajectories, each ranked by a conditional probability based on one or more environmental factors; determining, by a distance prediction module of the trained machine learning prediction module, a distance corresponding to each of the most probable descent flight trajectories; outputting, to a pilot, one or more of the most probable descent flight trajectories and the corresponding distances; determining a recommended top of descent location corresponding to the distance determined for the most probable descent flight trajectory based on a desired angle of descent and windspeed data of the predicted weather data; and outputting the recommended top of descent location to the pilot or to a flight director system of the aircraftâ s avionics for control of an associated autopilot system; wherein the trained machine learning prediction model is trained based on historical aircraft flight data.
2. The method of claim 1 , wherein outputting the recommended top of descent location the flight director system further comprises outputting, to the flight director system, the desired angle of descent.
3. The method of any preceding claim, wherein the determination of the predicted arrival route and the predicted landing runway by the first clustering module uses hierarchical clustering.
4. The method of any preceding claim, wherein the determination of the plurality of descent flight trajectories for the aircraft flight by the second clustering module uses density-based clustering.
5. The method of any preceding claim, where the trained machine learning prediction module is trained based on historical aircraft flight data only corresponding to the aircraft the aircraft flight.
6. The method of any preceding claim, wherein the one or more environmental factors comprise one or more of the time of day of the scheduled landing, the day of the week of the scheduled landing, the precipitation level in the vicinity of the destination aerodrome at the scheduled landing time, the visibility distance in the vicinity of the destination aerodrome at the scheduled landing time, the windspeed in the vicinity of the destination aerodrome at the scheduled landing time, or the wind direction in the vicinity of the destination aerodrome at the scheduled landing time.
7. A system for improving the fuel efficiency of an aircraft flight, the system comprising: a flight plan data store configured to store a flight plan for the aircraft flight, the flight plan comprising a scheduled route for the aircraft flight, a scheduled landing runway at a destination aerodrome, and a scheduled arrival time and date at the destination aerodrome; a weather data store configured to store predicted weather data corresponding to the vicinity of the airport at the scheduled arrival time and date; a trained machine learning prediction module that has trained based on historical aircraft flight data, the trained machine learning prediction module comprising: a first cluster mapping module configured to receive the scheduled route for the aircraft flight, the scheduled landing runway at a destination aerodrome, and the predicted weather data corresponding to the vicinity of the destination aerodrome at the scheduled arrival time and date; the first cluster mapping module configured to determine, based on the trained machine learning of the prediction module, a predicted arrival route and a predicted landing runway; a second cluster mapping module configured to determine, based on the predicted arrival route and the predicted landing runway, a plurality of descent flight trajectories for the aircraft flight; a trajectory filter configured to filter the plurality of descent flight trajectories for the aircraft flight to obtain the most probable descent flight trajectories, each ranked by a conditional probability based on one or more environmental factors; and a distance prediction module configured to determine a distance corresponding to each of the most probable descent flight trajectories; and an output configured to output, to a pilot, one or more of the most probable descent flight trajectories and the corresponding distances; wherein the trained machine learning prediction module is further configured to recommend a top of descent location corresponding to the distance determined for the most probable descent flight trajectory based on a desired angle of descent and windspeed data of the predicted weather data; and wherein the output is further configured to output the recommended top of descent location to the pilot or to a flight director system of the aircraftâ s avionics for control of an associated autopilot system.
8. The system of claim 7, wherein the output is further configured to output, to the flight director system the desired angle of descent.
9. The system of claim 7 or 8, wherein the first clustering module is configured to use hierarchical clustering to determine the predicted arrival route and the predicted landing runway.
10. The system of any of claims 7 to 9, wherein the second clustering module is configured to use density-based clustering to determine the plurality of descent flight trajectories for the aircraft flight.
11 . The system of any of claims 7 to 10, wherein the trained machine learning prediction module is trained based on historical aircraft flight data only corresponding to the aircraft the aircraft flight.
12. The system of any of claims 7 to 11 , wherein the one or more environmental factors comprise one or more of the time of day of the scheduled landing, the day of the week of the scheduled landing, the precipitation level in the vicinity of the destination aerodrome at the scheduled landing time, the visibility distance in the vicinity of the destination aerodrome at the scheduled landing time, the windspeed in the vicinity of the destination aerodrome at the scheduled landing time, or the wind direction in the vicinity of the destination aerodrome at the scheduled landing time.
13. A method for training a machine learning module to predict the most probable descent flight trajectories, the method comprising: receiving an indication of a planned route for a plurality of historic aircraft flights; receiving, for each historic aircraft flight, recorded flight data from the aircraft, the recorded flight data comprising aircraft position data and aircraft heading data, the position data forming a trajectory for each aircraft flight of the plurality of historic aircraft flights; receiving an indication of the magnetic bearing of each runway of a plurality of runways at a destination aerodrome; determining, for each historic aircraft flight, which runway was used for landing of the plurality of runways at the destination aerodrome, and what the approach direction to that runway was, based on the aircraft position data and/or the aircraft heading data; performing a first cluster analysis, at a first clustering module of the machine learning module, configured to group trajectories having the same determined landing runway and approach direction into a plurality of clusters; performing, for each of the plurality of clusters, a second cluster analysis, at a second clustering module of the machine learning module, configured to group trajectories based on the distance between respective trajectories to determine a consolidated set of trajectories; and determining, for each consolidated set of trajectories, at a regression module, a conditional probability based on one or more environmental factors.
14. The method of claim 13, wherein the machine learning module is trained based on historical aircraft flight data corresponding to a single aircraft.
15. The method of claim 13 or 14, wherein the first cluster analysis and the second cluster analysis are based on one or more geospatial algorithms.
16. The method of any of claims 13 to 15, wherein the first cluster analysis is based on hierarchical clustering.
17. The method of any of claims 13 to 16, wherein the second cluster analysis is based on density-based clustering.
18. The method of any of claims 13 to 17, wherein the one or more environmental factors comprise one or more of the time of day of the scheduled landing, the day of the week of the scheduled landing, the precipitation level in the vicinity of the destination aerodrome at the scheduled landing time, the visibility distance in the vicinity of the destination aerodrome at the scheduled landing time, the windspeed in the vicinity of the destination aerodrome at the scheduled landing time, or the wind direction in the vicinity of the destination aerodrome at the scheduled landing time.
19. A method for predicting the optimum parameters for a fuel efficient aircraft descent phase, the method comprising: training a machine learning module by: receiving, for each of a plurality of historic aircraft flights, recorded flight data from the aircraft, the recorded flight data comprising aircraft fuel consumption data, aircraft vertical speed data, aircraft indicated airspeed data, altitude based windspeed data, and altitude based ambient temperature data; dividing a descent altitude into a plurality of altitude subsections; determining, for each altitude subsection of each of the plurality of historic aircraft flights, the time taken and the amount of fuel consumption for the aircraft to descend through the altitude subsection based on the recorded flight data; and associating each altitude subsection of each of the plurality of historic aircraft flights with the recorded windspeed, the ambient temperature and the aircraftâ s indicated airspeed or Mach airspeed; for a future aircraft descent having a specified flight plan data and predicted altitude based weather data, iteratively stepping through the descent speeds for each altitude subsection, and performing a prediction, using the trained machine learning module, of the overall time taken and fuel consumed for each descent speed; and comparing the predictions and selecting the altitude subsection descent speeds associated with the lowest fuel consumption and within a desired flight time range.
20. The method of claim 19, wherein the machine learning module is trained based on historical aircraft flight data only corresponding to an individual aircraft, with subsequent predictions corresponding to the individual aircraft.
21 . The method of claim 19 or 20, wherein the flight plan data comprises the flight cruise level, the planned take-off weight, and the scheduled date and time of arrival.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR20225974 | 2022-06-17 | ||
| PCT/EP2023/066336 WO2023242433A1 (en) | 2022-06-17 | 2023-06-16 | A system and method for optimising flight efficiency |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB202500657D0 GB202500657D0 (en) | 2025-03-05 |
| GB2635621A true GB2635621A (en) | 2025-05-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2500657.8A Pending GB2635621A (en) | 2022-06-17 | 2023-06-16 | A system and method for optimising flight efficiency |
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| Country | Link |
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| GB (1) | GB2635621A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140358415A1 (en) * | 2011-12-06 | 2014-12-04 | Airservices Australia | Flight prediction system |
| US9193442B1 (en) * | 2014-05-21 | 2015-11-24 | Rockwell Collins, Inc. | Predictable and required time of arrival compliant optimized profile descents with four dimensional flight management system and related method |
| US20150338853A1 (en) * | 2014-05-23 | 2015-11-26 | The Boeing Company | Determining a descent trajectory described by an Aircraft Intent Description Language (AIDL) |
| US9423799B1 (en) * | 2013-08-12 | 2016-08-23 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration (Nasa) | Optimum strategies for selecting descent flight-path angles |
| US20190371187A1 (en) * | 2018-06-05 | 2019-12-05 | Honeywell International Inc. | Methods and systems for stabilized approach energy management |
| US10643480B2 (en) * | 2016-04-19 | 2020-05-05 | George Mason University | Method and apparatus for probabilistic alerting of aircraft unstabilized approaches using big data |
| US10678265B2 (en) * | 2016-10-19 | 2020-06-09 | Airbus Sas | Revised speed advisory for an aircraft during flight based on holding time |
| US20200183427A1 (en) * | 2018-12-06 | 2020-06-11 | Airbus Operations (S.A.S.) | Method and avionic system for generating an optimum vertical trajectory |
| US20210233415A1 (en) * | 2015-07-13 | 2021-07-29 | Double Black Aviation Technology L.L.C. | System and method for optimizing an aircraft trajectory |
-
2023
- 2023-06-16 GB GB2500657.8A patent/GB2635621A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140358415A1 (en) * | 2011-12-06 | 2014-12-04 | Airservices Australia | Flight prediction system |
| US9423799B1 (en) * | 2013-08-12 | 2016-08-23 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration (Nasa) | Optimum strategies for selecting descent flight-path angles |
| US9193442B1 (en) * | 2014-05-21 | 2015-11-24 | Rockwell Collins, Inc. | Predictable and required time of arrival compliant optimized profile descents with four dimensional flight management system and related method |
| US20150338853A1 (en) * | 2014-05-23 | 2015-11-26 | The Boeing Company | Determining a descent trajectory described by an Aircraft Intent Description Language (AIDL) |
| US20210233415A1 (en) * | 2015-07-13 | 2021-07-29 | Double Black Aviation Technology L.L.C. | System and method for optimizing an aircraft trajectory |
| US10643480B2 (en) * | 2016-04-19 | 2020-05-05 | George Mason University | Method and apparatus for probabilistic alerting of aircraft unstabilized approaches using big data |
| US10678265B2 (en) * | 2016-10-19 | 2020-06-09 | Airbus Sas | Revised speed advisory for an aircraft during flight based on holding time |
| US20190371187A1 (en) * | 2018-06-05 | 2019-12-05 | Honeywell International Inc. | Methods and systems for stabilized approach energy management |
| US20200183427A1 (en) * | 2018-12-06 | 2020-06-11 | Airbus Operations (S.A.S.) | Method and avionic system for generating an optimum vertical trajectory |
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| Publication number | Publication date |
|---|---|
| GB202500657D0 (en) | 2025-03-05 |
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