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Output Feedback Sliding Mode Control of a Fixed-Wing UAV Under Rudder Loss

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dc.contributor.authorKaẏnak, Ünver
dc.contributor.authorArtun Sel
dc.contributor.authorÇoşku Kasnakoğlu
dc.contributor.authorÜnver Kaẏnak
dc.contributor.orcid0000-0002-3142-3650
dc.contributor.orcid0000-0002-9928-727X
dc.date.accessioned2025-11-13T10:50:20Z
dc.date.issued2019-01-06
dc.identifier.doihttps://doi.org/10.2514/6.2019-0911
dc.identifier.openalexW2910665326
dc.identifier.urihttps://hdl.handle.net/11421/5412
dc.identifier.urihttps://doi.org/10.2514/6.2019-0911
dc.language.isoen
dc.relation.ispartofAIAA Scitech 2019 Forum
dc.rightsrestrictedAccess
dc.subjectRudder
dc.subjectFixed wing
dc.subjectControl theory (sociology)
dc.subjectWing
dc.subjectSliding mode control
dc.subjectMode (computer interface)
dc.subjectComputer science
dc.subjectFeedback control
dc.subjectControl (management)
dc.subjectControl engineering
dc.subjectEngineering
dc.subjectPhysics
dc.subjectAerospace engineering
dc.subjectNonlinear system
dc.subjectArtificial intelligence
dc.subject.sdg7
dc.titleOutput Feedback Sliding Mode Control of a Fixed-Wing UAV Under Rudder Loss
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5027789444

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