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

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® workflow, capable of providing a relatively simple sizing, but highly realistic airplane.

KEYWORDS:
Airplane design; Solar energy; Multi-disciplinary design and optimization; Airplane stability and control

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Publication Dates

  • Publication in this collection
    Jul-Sep 2013

History

  • Received
    17 Dec 2012
  • Accepted
    10 Apr 2013
Departamento de Ciência e Tecnologia Aeroespacial Instituto de Aeronáutica e Espaço. Praça Marechal do Ar Eduardo Gomes, 50. Vila das Acácias, CEP: 12 228-901, tel (55) 12 99162 5609 - São José dos Campos - SP - Brazil
E-mail: submission.jatm@gmail.com