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Flight Procedure Analysis for a Combined Environmental Impact Reduction: An Optimal Trade-Off Strategy
KTH, School of Engineering Sciences (SCI), Engineering Mechanics.ORCID iD: 0000-0001-9902-6216
2022 (English)In: Aerospace, E-ISSN 2226-4310, Vol. 9, no 11, p. 683-683Article in journal (Refereed) Published
Abstract [en]

Many attempts have been made to reduce aviation’s environmental impact, as aviation traffic has grown exponentially in recent decades. While some approaches focus on technology and fuel alternatives, others strive to develop improved operational measures within air traffic management as a short-term action to mitigate aviation-induced climate change, as well as air pollution. In this work, different flight procedures are analyzed in terms of emissions and noise impact to define optimal trade-offs. The investigation is based on flight data recorders, emissions, and noise prediction models. An aircraft trajectory simulation code with flight procedure optimization is also implemented to define an environmentally optimal trajectory. The results show that while noise and the emissions proportional to the burned fuel may be reduced for some trajectories, other non-CO2 emissions could drastically increase if too low idle-thrust levels are reached. Therefore, a minimum threshold for idle thrust is suggested as a key factor to define a truly optimal trajectory in terms of CO2 emissions, non-CO2 emissions, and noise.

Place, publisher, year, edition, pages
MDPI AG , 2022. Vol. 9, no 11, p. 683-683
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-321076DOI: 10.3390/aerospace9110683ISI: 000883363600001Scopus ID: 2-s2.0-85141879850OAI: oai:DiVA.org:kth-321076DiVA, id: diva2:1708687
Note

QC 20221108

Available from: 2022-11-04 Created: 2022-11-04 Last updated: 2022-12-02Bibliographically approved

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Otero, Evelyn

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