Trajectory optimization of extended formation flights for commercial aviation

This paper presents a trajectory optimization study that has been conducted using a recently developed tool for the synthesis and analysis of extended flight formations of long-haul commercial aircraft, with the aim to minimize overall fuel consumption. In extended flight formations, trailing aircra...

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Published in:Aerospace
Main Authors: Hartjes, S. (author), Visser, H.G. (author), Hubar, Marco E.G.van Hellenberg (author)
Format: Article in Journal/Newspaper
Language:English
Published: 2019
Subjects:
Online Access:http://resolver.tudelft.nl/uuid:8231f372-5cb7-48f0-9cf6-c31f73d9585c
https://doi.org/10.3390/aerospace6090100
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author Hartjes, S. (author)
Visser, H.G. (author)
Hubar, Marco E.G.van Hellenberg (author)
author_facet Hartjes, S. (author)
Visser, H.G. (author)
Hubar, Marco E.G.van Hellenberg (author)
author_sort Hartjes, S. (author)
collection Delft University of Technology: Institutional Repository
container_issue 9
container_start_page 100
container_title Aerospace
container_volume 6
description This paper presents a trajectory optimization study that has been conducted using a recently developed tool for the synthesis and analysis of extended flight formations of long-haul commercial aircraft, with the aim to minimize overall fuel consumption. In extended flight formations, trailing aircraft can attain an appreciable reduction in induced drag and associated reduction in fuel burn by flying in the upwash of the lead aircraft's wake. In the present study, a previously developed multi-phase optimal control (MOC) framework for the synthesis of two-ship flight formations has been extended to include the assembly of three-ship flight formations. Using the extended tool, various numerical experiments have been conducted in relation to the assembly of two-ship and three-ship flight formations in long-haul operations across the North-Atlantic Ocean. Additionally, numerical experiments have been carried out to examine the impact of wind fields on the synthesis and performance of flight formations. Additionally, a parametric investigation has been conducted to assess the sensitivity of the solutions with respect to the degree of the induced drag reduction that might be attained by the trailing aircraft in a formation. The results of the various numerical experiments reveal that formation flight can result in appreciable reductions in fuel burn in comparison to flying solo-particularly when larger formation strings are permitted. Air Transport & Operations
format Article in Journal/Newspaper
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op_rights © 2019 S. Hartjes, H.G. Visser, Marco E.G.van Hellenberg Hubar
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spelling fttudelft:oai:tudelft.nl:uuid:8231f372-5cb7-48f0-9cf6-c31f73d9585c 2025-01-16T23:41:44+00:00 Trajectory optimization of extended formation flights for commercial aviation Hartjes, S. (author) Visser, H.G. (author) Hubar, Marco E.G.van Hellenberg (author) 2019-09-01 http://resolver.tudelft.nl/uuid:8231f372-5cb7-48f0-9cf6-c31f73d9585c https://doi.org/10.3390/aerospace6090100 en eng http://www.scopus.com/inward/record.url?scp=85072208810&partnerID=8YFLogxK Aerospace--2226-4310--098c216f-9158-4b61-bb99-8669758314ff http://resolver.tudelft.nl/uuid:8231f372-5cb7-48f0-9cf6-c31f73d9585c https://doi.org/10.3390/aerospace6090100 © 2019 S. Hartjes, H.G. Visser, Marco E.G.van Hellenberg Hubar Flight formations Fuel burn Trajectory optimization Wind fields journal article 2019 fttudelft https://doi.org/10.3390/aerospace6090100 2024-04-09T23:55:06Z This paper presents a trajectory optimization study that has been conducted using a recently developed tool for the synthesis and analysis of extended flight formations of long-haul commercial aircraft, with the aim to minimize overall fuel consumption. In extended flight formations, trailing aircraft can attain an appreciable reduction in induced drag and associated reduction in fuel burn by flying in the upwash of the lead aircraft's wake. In the present study, a previously developed multi-phase optimal control (MOC) framework for the synthesis of two-ship flight formations has been extended to include the assembly of three-ship flight formations. Using the extended tool, various numerical experiments have been conducted in relation to the assembly of two-ship and three-ship flight formations in long-haul operations across the North-Atlantic Ocean. Additionally, numerical experiments have been carried out to examine the impact of wind fields on the synthesis and performance of flight formations. Additionally, a parametric investigation has been conducted to assess the sensitivity of the solutions with respect to the degree of the induced drag reduction that might be attained by the trailing aircraft in a formation. The results of the various numerical experiments reveal that formation flight can result in appreciable reductions in fuel burn in comparison to flying solo-particularly when larger formation strings are permitted. Air Transport & Operations Article in Journal/Newspaper North Atlantic Delft University of Technology: Institutional Repository Aerospace 6 9 100
spellingShingle Flight formations
Fuel burn
Trajectory optimization
Wind fields
Hartjes, S. (author)
Visser, H.G. (author)
Hubar, Marco E.G.van Hellenberg (author)
Trajectory optimization of extended formation flights for commercial aviation
title Trajectory optimization of extended formation flights for commercial aviation
title_full Trajectory optimization of extended formation flights for commercial aviation
title_fullStr Trajectory optimization of extended formation flights for commercial aviation
title_full_unstemmed Trajectory optimization of extended formation flights for commercial aviation
title_short Trajectory optimization of extended formation flights for commercial aviation
title_sort trajectory optimization of extended formation flights for commercial aviation
topic Flight formations
Fuel burn
Trajectory optimization
Wind fields
topic_facet Flight formations
Fuel burn
Trajectory optimization
Wind fields
url http://resolver.tudelft.nl/uuid:8231f372-5cb7-48f0-9cf6-c31f73d9585c
https://doi.org/10.3390/aerospace6090100