Conceptual Design of Green Propulsive Systems Using Reinforcement Learning

Hybrid-electric powertrains offer a solution to significantly reduce aircraft emissions in flight. This study presents a method for automatically generating hybrid-electric architectures and optimizes their control parameters to maximize payload using reinforcement learning. Applied to an ATR 72-600 reference aircraft, with the Flightpath 2050 sustainability goals as constraints, the framework indentifies an optimal architecture: a gas turbine combusting conventional jet fuel and hydrogen powers the primary propulsive line, while fuel cells deliver the majority of the power to an auxiliary propulsive line. Compared with a conventional architecture, this design reduces CO2 and NOx emissions by up to 74% and 86%, respectively, incurring a payload mass penalty of only 24%.

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Publication Details

Journal
Aerospace
Published
2026-08-26
DOI
https://doi.org/10.3390/aerospace13090763
Primary Topic
Advanced Aircraft Design and Technologies
Type
article
Field-Weighted Citation Impact
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article

Conceptual Design of Green Propulsive Systems Using Reinforcement Learning

Francesco Orefice, Martijn van Dongeren
Aerospace
Advanced Aircraft Design and Technologies
article

Conceptual Design of Green Propulsive Systems Using Reinforcement Learning

Francesco Orefice, Martijn van Dongeren
article en

Abstract

Hybrid-electric powertrains offer a solution to significantly reduce aircraft emissions in flight. This study presents a method for automatically generating hybrid-electric architectures and optimizes their control parameters to maximize payload using reinforcement learning. Applied to an ATR 72-600 reference aircraft, with the Flightpath 2050 sustainability goals as constraints, the framework indentifies an optimal architecture: a gas turbine combusting conventional jet fuel and hydrogen powers the primary propulsive line, while fuel cells deliver the majority of the power to an auxiliary propulsive line. Compared with a conventional architecture, this design reduces CO2 and NOx emissions by up to 74% and 86%, respectively, incurring a payload mass penalty of only 24%.

AerospaceVol. 13(9)
Openalex Percentile: Top 36%
Advanced Aircraft Design and Technologies
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