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Modelling and Experimental Validation of a Hybrid Electric Propulsion System for Light Aircraft and Unmanned Aerial Vehicles

This article presents a numerical model of an aeronautical hybrid electric propulsion system (HEPS) based on an energy method. This model is designed for HEPS with a total power of 100 kW in a parallel configuration intended for ultralight aircraft and unmanned aerial vehicles (UAV). The model invol...

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Principais autores: Massimo Cardone, Bonaventura Gargiulo, Enrico Fornaro
Format: Artigo
Sprog:Inglês
Udgivet: MDPI AG 2021-07-01
Serier:Energies
Fag:
hybrid electric propulsion system
parallel configuration
unmanned aerial vehicle
experimental validation
MATLAB Simulink simulation
aircraft
Online adgang:https://www.mdpi.com/1996-1073/14/13/3969
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