No AccessNew methodology for the controller of an electrical actuator for morphing a wingMichel Joel Tchatchueng Kammegne, Shehryar Khan and Ruxandra BotezMichel Joel Tchatchueng KammegneÉcole de Technologie SupérieureSearch for more papers by this author, Shehryar KhanÉcole de Technologie SupérieureSearch for more papers by this author and Ruxandra BotezÉcole de Technologie SupérieureSearch for more papers by this authorAIAA 2015-1256Session: Adaptive ActuationPublished Online:2 Jan 2015https://doi.org/10.2514/6.2015-1256SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byA New Method for Tuning PI Gains for Position Control of BLDC Motor Based Wing Morphing ActuatorsRuxandra M. Botez, Shehryar Khan and Teordor L. Grigorie18 June 2015 What's Popular 23rd AIAA/AHS Adaptive Structures Conference 5-9 January 2015Kissimmee, Floridahttps://doi.org/10.2514/6.2015-1256 CrossmarkInformationCopyright © 2015 by Ruxandra Mihaela Botez. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAircraft Components and StructureAircraft DesignAircraft Operations and TechnologyAircraft Stability and ControlAircraft Wing DesignAircraftsAirfoilAirfoil NomenclatureFixed-Wing AircraftFlight Control SurfacesLongitudinal Static StabilityWing Configurations KeywordsLinear ActuatorLift to Drag RatioProportional Integral DerivativeElectromotive ForcesAerodynamic PropertiesPiezoelectric MaterialsWind Tunnel TestsNumerical AnalysisFinite Element AnalysisAeroservoelasticityPDF Topics Adaptive Structures