Optimal Design of a High-Altitude Solar-Powered Unmanned Airplane

Author(s)

de Mattos, Bento Silva ; Secco, Ney Rafael ; Salles, Eduardo Francisco

• Document type: Journal article
• Source: JOURNAL OF AEROSPACE TECHNOLOGY AND MANAGEMENT; v. 5, n. 3, p. 13-pg., 2013-07-01.

Abstract

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 (R) workflow, capable of providing a relatively simple sizing, but highly realistic airplane. (AU)

• FAPESP's process: 07/00305-5 - High-performance numerical simulation applied to aircraft design and optimization
• Grantee: Nide Geraldo do Couto Ramos Fico Júnior
• Support Opportunities: Regular Research Grants