Automation of conceptual design and modification of aircraft type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 1: Methods and models

This paper proposes a method for selecting rational parameters for large-size aircraft-type unmanned aerial vehicles at the initial design stages using an optimization algorithm of differential evolution and numerical mathematical modeling of aerodynamic problems. The method assumes implementation o...

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Detalhes bibliográficos

Principais autores:	V. A. Komarov, O. E. Lukyanov, V. H. Hoang, E. I. Kurkin, J. G. QuijadaPioquinto
Formato:	Artigo
Idioma:	Inglês
Publicado em:	Samara National Research University 2024-10-01
coleção:	Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Assuntos:	unmanned aerial vehicle appearance design takeoff weight optimization evolutionary algorithm aerodynamics balancing penalty function parallel computing
Acesso em linha:	https://journals.ssau.ru/vestnik/article/viewFile/27907/10831
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