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Atmospheric Aircraft Conceptual Design Based on Multidisciplinary Optimization with Differential Evolution Algorithm and Neural Networks

A methodology for selecting rational parameters of atmospheric aircraft during the initial design stages using a differential evolutionary optimization algorithm and numerical mathematical modeling of aerodynamics problems is proposed. The technique involves implementing weight and aerodynamic balan...

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Principais autores: Oleg Lukyanov, Van Hung Hoang, Evgenii Kurkin, Jose Gabriel Quijada-Pioquinto
Format: Artigo
Sprog:Inglês
Udgivet: MDPI AG 2024-08-01
Serier:Drones
Fag:
atmospheric aircraft
appearance
design
takeoff weight
optimization
differential evolution algorithm
Online adgang:https://www.mdpi.com/2504-446X/8/8/388
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