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A Stabilizing Controller for PVTOL Aircraft

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dc.contributor.authorTurker, Turker
dc.contributor.authorOflaz, Tugce
dc.contributor.authorGorgun, Haluk
dc.contributor.authorCansever, Galip
dc.date.accessioned2026-06-27T13:19:39Z
dc.date.issued2012
dc.description.abstractA stabilizing controller structure is proposed for planar vertical take off and landing (PVTOL) aircraft. In order to achieve almost global asymptotic stabilization, the coupling coefficient, is an element of, is assumed to be in the interval 0 <= is an element of < 1. Stability analysis is performed based on a Lyapunov function and asymptotic convergence is proven by means of La Salle's invariance principle. The proposed controller is implemented by numerical simulations on PVTOL aircraft and results are presented.en
dc.identifier.eissn2378-5861
dc.identifier.endpage913
dc.identifier.isbn978-1-4577-1096-4; 978-1-4577-1095-7
dc.identifier.issn0743-1619
dc.identifier.startpage909
dc.identifier.urihttps://hdl.handle.net/20.500.14981/51861
dc.identifier.wos000310776201031
dc.language.isoeng
dc.publisherIEEE COMPUTER SOC
dc.relation.conferenceAmerican Control Conference (ACC)
dc.relation.ispartof2012 AMERICAN CONTROL CONFERENCE (ACC)
dc.subjectGLOBAL STABILIZATION
dc.subjectSYSTEMS
dc.subjectAutomation & Control Systems
dc.subjectEngineering
dc.titleA Stabilizing Controller for PVTOL Aircraft
dc.typeProceedings Paper
dspace.entity.typePublication
local.import.sourceWOS

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