Intelligent control of a morphing wing Part 1: Design phase

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.2316/P.2011.715-053
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Affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
ConferenceIASTED International Conference on Applied Simulation and Modelling, ASM 2011, 22 June 2011 through 24 June 2011, Crete
SubjectController architectures; Fuzzy logic control; Fuzzy logic controllers; Intelligent controllers; Laminar to turbulent transitions; Morphing wings; Proportional-integral; Shape memory alloys(SMA); Fuzzy logic; Intelligent control; Modal analysis; Wind tunnels; Membership functions
Abstract
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LanguageEnglish
Peer reviewedYes
NPARC number21271094
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Record identifierfcbe1d9d-025b-44cd-876b-e882451f45e3
Record created2014-03-24
Record modified2020-04-21
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