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Aircraft Control via Variable Cant-Angle Winglets / P Bourdin; A Gatto; M. I Friswell; Michael Friswell

Journal of Aircraft, Volume: 45, Issue: 2, Pages: 414 - 423

Swansea University Author: Michael, Friswell

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DOI (Published version): 10.2514/1.27720

Published in: Journal of Aircraft
ISSN: 0021-8669 1533-3868
Published: 2008
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URI: https://cronfa.swan.ac.uk/Record/cronfa5504
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Item Description: This paper formed part of the Marie-Curie Excellence grant on morphing aircraft (1.94M euros, 2005-2008) and was the first to consider using active winglets as control effectors. The investigation highlighted that novel aircraft configurations departed from the standard flight control approach of decoupling degrees of freedom and required a system view of such aircraft. This system level thinking was vital to the concept of the ERC Advanced Investigator grant on morphing aircraft (2.5M euros, 2010-2015).
College: College of Engineering
Issue: 2
Start Page: 414
End Page: 423