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dc.contributor.authorMARTIN, Mikael
dc.contributor.authorBARRE, Pierre-Jean
dc.contributor.author
 hal.structure.identifier
GOMAND, Julien
178374 Laboratoire des Sciences de l'Information et des Systèmes : Ingénierie Numérique des Systèmes Mécaniques [LSIS- INSM]
dc.contributor.authorMALBURET, François
dc.date.accessioned2014
dc.date.available2014
dc.date.issued2012
dc.date.submitted2014
dc.identifier.isbn978-1-4673-3142-5
dc.identifier.urihttp://hdl.handle.net/10985/8963
dc.description.abstractA helicopter flight axis control, which is a complex multi-physic system, is modelled using an energetic based graphical tool: the Energetic Macroscopic Representation. Elements of the system are mainly composed of passive technologies and their number tends to increase year after year to improve the pilots comfort by adding new functions. A new methodology is proposed to transform the system into a new active one by replacing some hydro-mechanical elements by a new controllable active mechanical source. The challenge is to simplify the flight control architecture while preserving the global behaviour of the system.
dc.language.isoen
dc.publisherIEEE
dc.rightsPost-print
dc.subjectEnergetic Macroscopic Representation
dc.subjectHelicopter
dc.subjectInternal Model Reference
dc.subjectTerms — Energetic Macroscopic Representation
dc.titleMulti-physic system simplification method applied to a helicopter flight axis active control
dc.identifier.doi10.1109/ICCSCE.2012.6487155
dc.typdocCommunication avec acte
dc.localisationCentre de Aix en Provence
dc.subject.halSciences de l'ingénieur: Automatique / Robotique
dc.subject.halSciences de l'ingénieur: Mécanique
ensam.audienceInternationale
ensam.conference.titleMulti-Physic System Simplification Method Applied to a Helicopter Flight Axis Active Control
ensam.conference.date2012-11-23
ensam.countryMalaysia
ensam.title.proceedingControl System, Computing and Engineering (ICCSCE)
ensam.page274 - 279
ensam.cityPenang
hal.identifierhal-01086078
hal.version1
hal.submission.permittedupdateMetadata
hal.statusaccept


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