Artigo
2013
Optimal design of a high-altitude solar-powered unmanned airplane
Autores
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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2-s2.0-84884148651
