Design of a Hybrid Digital-Twin Flight Performance Model Through Machine Learning

Mevlut Uzun, M. Umut Demirezen, Emre Koyuncu, Gokhan Inalhan

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

11 Citations (Scopus)

Abstract

This study implements deep learning techniques to estimate fuel burn of a jet aircraft. Current ground-based flight planning systems utilize aircraft type specific performance tables to determine fuel flows for given flight conditions and parameters such as altitude, mass and speed. These tables are corrected by a performance factor as the aircraft ages. Despite this update, planned fuel consumption may indeed not overlap with the actual one. In order to synchronize the base aircraft model with aircraft's actual performance, we propose using state-of-the-art deep learning algorithms for building data-driven models of fuel flows. Towards this goal, aircraft's on-board recorded trajectory and parameter data, namely Quick Access Recorder (QAR) data are utilized. The total dataset used within this study comprises of more than 1000 B777-300ER flights from a major European flag carrier airline. The deep neural network architecture is utilized for modeling the actual fuel flow specific to each aircraft and for each major flight mode (climb, cruise and descent namely). We have developed three neural network architectures (according to in-flight and ground based planning use cases) to present a tail-number specific correction factor to Base of Aircraft Data (BADA) models. First architecture involves a QAR data based black-box fuel flow model utilizing in-flight throttle data from all the engines. Comparison of this model with real flight data shows that precise estimation of fuel flow with mean errors lower than %0.1 can be achieved. The second architecture utilizes a physically consistent data regeneration of \delta-{T} (delta thrust) using BADA formulation as to account for the ground planning phase where throttle information is not available. The third model involves a cascaded architecture which utilizes a neural network throttle estimator and the black-box QAR fuel flow model for again the ground planning phase. Comparison of the latter models with real flight data shows that precise estimation of fuel flow with mean absolute errors lower than %0.7 can be achieved at all the flight modes. Initial tests reflect the fact that even better accuracy can be achieved for all models as the data set size increases. Finally, ground based planning fuel flow models are applied to actual flight plans generated by ground based systems. Total trip fuel comparisons show discrepancies up to %3.5 total fuel loading weight, which may result in potential fuel savings by decreasing the fuel load during take-off. Comparison of the planned and the estimated fuel boarding weights (following the actual filed flight plans) for 91 long-haul flights show that fuel burn savings of around 800 [k g] per flight could have been achieved by the proposed methodology at the ground planning phase. For a typical operation of 100 long-haul flights per day, this represents yearly savings on the order of around 17 million USD at current jet fuel prices. This 'tail-number specific' performance modeling approach is projected to open considerable frontiers including the in-flight update of performance models through machine learning methods.

Original languageEnglish
Title of host publication2019 IEEE Aerospace Conference, AERO 2019
PublisherIEEE Computer Society
ISBN (Electronic)9781538668542
DOIs
Publication statusPublished - Mar 2019
Event2019 IEEE Aerospace Conference, AERO 2019 - Big Sky, United States
Duration: 2 Mar 20199 Mar 2019

Publication series

NameIEEE Aerospace Conference Proceedings
Volume2019-March
ISSN (Print)1095-323X

Conference

Conference2019 IEEE Aerospace Conference, AERO 2019
Country/TerritoryUnited States
CityBig Sky
Period2/03/199/03/19

Bibliographical note

Publisher Copyright:
© 2019 IEEE.

Funding

This work is partially funded under Boeing grant 2016-621-1. The authors would like to thank the Turkish Airlines for their support within this work.

FundersFunder number
Boeing2016-621-1

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