Performance Evaluation of an H-VTOL Aircraft with Distributed Electric Propulsion and Ducted-Fans Using MIL Simulation

Performance Evaluation of an H-VTOL Aircraft with Distributed Electric Propulsion and Ducted-Fans Using MIL Simulation

This paper deals with the problem of increasing the energy efficiency of a hybrid vertical take-off and landing aircraft. To this end, an innovative aerial vehicle was developed, featuring a distributed electrical propulsion system with ducted-fan rotors. To compare and analyze the effectiveness of...

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Bibliographic Details
Main Authors: Juan Manuel Bustamante Alarcon, José Leonel Sánchez Marmolejo, Luis Héctor Manjarrez Muñoz, Eduardo Steed Espinoza Quesada, Antonio Osorio Cordero, Luis Rodolfo García Carrillo
Format: Article
Language:English
Published: MDPI AG 2023-08-01
Series:Machines
Subjects:
distributed electric propulsion
VTOL
model-in-the-loop simulation
X-plane
ducted-fan
unmanned aircraft system
Online Access:https://www.mdpi.com/2075-1702/11/9/852

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