Design and experimental testing of a control system for a morphing wing model actuated with miniature BLDC motors

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DOIResolve DOI: https://doi.org/10.1016/j.cja.2019.08.007
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Affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
SubjectBLDC motor; control tuning; morphing wing; simulation and experimental testing; wind tunnel
Abstract
Publication date
PublisherElsevier
Chinese Society of Aeronautics and Astronautics
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In
LanguageEnglish
Peer reviewedYes
IdentifierS100093611930305X
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Record identifiercf506f82-2b34-4ca5-8e0d-dd034b90a41e
Record created2021-04-16
Record modified2021-04-21
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