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A hybrid fuzzy logic proportional integral derivative plus conventional on-off controller for a morphing wing actuation using shape memory alloys

From National Research Council Canada

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Affiliation
  1. National Research Council Canada. Aerospace
FormatText, Article
Conference52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, April 4-7, 2011, Denver, Colorado, USA
Publication date
In
  • 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference [Proceedings].
LanguageEnglish
Peer reviewedYes
NPARC number23001790
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Record identifier0cda0957-cb1b-4163-aabd-0d46f668f7be
Record created2017-04-07
Record modified2020-07-14
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