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Stabilization of uncoupled PVTOL aircraft based on a Lyapunov function

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dc.contributor.authorTurker, Turker
dc.contributor.authorGorgun, Haulk
dc.contributor.authorCansever, Galip
dc.date.accessioned2026-06-27T13:16:03Z
dc.date.issued2012
dc.description.abstractIn this paper we present a stabilization procedure for PVTOL (planar vertical take off and landing) aircraft with zero coupling coefficient that is defined as the effect of rolling moment on lateral acceleration. A stabilizing control structure has been designed via Lyapunov's direct method including almost the whole state space and its asymptotic convergence has been proven using La Salle's invariance principle. Simulation results have illustrated the effectiveness of proposed control algorithm.en
dc.description.sponsorshipYildiz Technical University - BAPK [2010-04-02-KAP01]
dc.description.urihttps://doi.org/10.1177/0142331211408638
dc.identifier.doi10.1177/0142331211408638
dc.identifier.eissn1477-0369
dc.identifier.endpage584
dc.identifier.issn0142-3312
dc.identifier.issue5
dc.identifier.startpage578
dc.identifier.urihttps://hdl.handle.net/20.500.14981/51246
dc.identifier.volume34
dc.identifier.wos000304884400008
dc.language.isoeng
dc.publisherSAGE PUBLICATIONS LTD
dc.relation.ispartofTRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL
dc.subjectLa Salle's invariance principle
dc.subjectLyapunov-based control design
dc.subjectPVTOL aircraft
dc.subjectGLOBAL STABILIZATION
dc.subjectSYSTEMS
dc.subjectAutomation & Control Systems
dc.subjectInstruments & Instrumentation
dc.titleStabilization of uncoupled PVTOL aircraft based on a Lyapunov function
dc.typeArticle
dspace.entity.typePublication
local.import.sourceWOS

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