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Model derivation, attitude control and Kalman filter estimation of a quadcopter

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dc.contributor.authorKaba, Aziz
dc.contributor.authorErmeydan, Ahmet
dc.contributor.authorKıyak, Emre
dc.contributor.orcid0000-0003-0453-2912
dc.contributor.orcid0000-0002-6184-6363
dc.contributor.orcid0000-0002-5253-3613
dc.date.accessioned2025-11-13T10:14:28Z
dc.date.issued2017-04-01
dc.identifier.doihttps://doi.org/10.1109/iceee2.2017.7935821
dc.identifier.openalexW2621318417
dc.identifier.urihttps://hdl.handle.net/11421/3551
dc.identifier.urihttps://doi.org/10.1109/iceee2.2017.7935821
dc.language.isoen
dc.rightsrestrictedAccess
dc.subjectQuadcopter
dc.subjectControl theory (sociology)
dc.subjectKalman filter
dc.subjectLinearization
dc.subjectExtended Kalman filter
dc.subjectAttitude control
dc.subjectController (irrigation)
dc.subjectComputer science
dc.subjectControl engineering
dc.subjectNoise (video)
dc.subjectMATLAB
dc.subjectState space
dc.subjectEngineering
dc.subjectNonlinear system
dc.subjectMathematics
dc.subjectControl (management)
dc.subjectArtificial intelligence
dc.titleModel derivation, attitude control and Kalman filter estimation of a quadcopter
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5002078556
local.authorid.openalexA5088954278
local.authorid.openalexA5041694956

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