PG-EAM - Programa de Pós-Graduação em Engenharia Aeronáutica e Mecânica
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Artigo 2013

Optimal design of a high-altitude solar-powered unmanned airplane

Autores

de Mattos, Bento Silva
Salles, Eduardo Francisco

Journal of Aerospace Technology and Management , vol. 5 , no. 3 , pp. 349-361

ISSN: 19849648

29
Citações
3
Autores

Resumo

This paper describes a multi-disciplinary design and optimization framework tailored for the conceptual development of high-altitude solar-powered unmanned aerial vehicles. The aircraft baseline configuration that the framework is able to handle is very similar to that of Zephyr, which is developed by the UK based company QinetiQ. The disciplines of aerodynamics, structures, stability, weight, and systems were considered and integrated into a modeFrontier® workflow, capable of providing a relatively simple sizing, but highly realistic airplane.

Palavras-chave

Airplane design Airplane stability and control Multi-disciplinary design and optimization Solar energy

Aerospace Engineering (ENGI) Engineering (all) (ENGI)
: Scopus
Última atualização: 2026-06-25
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