Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/5906
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dc.contributor.authorBatmaz, Anıl Ufuk-
dc.contributor.authorElbir O.-
dc.contributor.authorKasnakoğlu, Coşku-
dc.date.accessioned2021-09-11T15:20:42Z-
dc.date.available2021-09-11T15:20:42Z-
dc.date.issued2013en_US
dc.identifier.citation32nd IASTED International Conference on Modelling, Identification and Control, MIC 2013, 11 February 2013 through 13 February 2013, Innsbruck, 96248en_US
dc.identifier.isbn9780889869431-
dc.identifier.issn1025-8973-
dc.identifier.urihttps://doi.org/10.2316/P.2013.794-060-
dc.identifier.urihttps://hdl.handle.net/20.500.11851/5906-
dc.description.abstractUnmanned Aerial Vehicles (UAVs) are currently one of the hot topics of study which have numerous applications such as remote sensing, aerial surveillance, exploration, search and rescue, transport, scientific research and armed attacks. In this work we consider a test-bed for the design of a low cost flight controller for a quadrotor and we demonstrate the design of the roll and pitch controllers on an experimental setup through the stages of data collection, modeling, control design and verification. The procedure consists of four stages: 1) Experimental determination of controller coefficients, 2) Data collection, 3) System identification, 4) Controller redesign by tuning coefficients with a numerical search. It is observed that the system designed as such is capable of achieving satisfactory pitch and roll stabilization, and coefficient tuning on the identified model noticeably improves the settling time and steady state oscillation amplitude.en_US
dc.language.isoenen_US
dc.relation.ispartofProceedings of the IASTED International Conference on Modelling, Identification and Controlen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectAerial vehiclesen_US
dc.subjectDiscrete timeen_US
dc.subjectFour rotor helicopteren_US
dc.subjectLinear estimationen_US
dc.subjectQuadrotoren_US
dc.subjectUAVen_US
dc.subjectVehicle controlen_US
dc.titleQuadrotor roll and pitch stabilization using system identification based redesign of empirical controllersen_US
dc.typeConference Objecten_US
dc.departmentFaculties, Faculty of Engineering, Department of Electrical and Electronics Engineeringen_US
dc.departmentFakülteler, Mühendislik Fakültesi, Elektrik ve Elektronik Mühendisliği Bölümütr_TR
dc.identifier.startpage293en_US
dc.identifier.endpage297en_US
dc.identifier.scopus2-s2.0-84875776058en_US
dc.institutionauthorKasnakoğlu, Coşku-
dc.identifier.doi10.2316/P.2013.794-060-
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.relation.conference32nd IASTED International Conference on Modelling, Identification and Control, MIC 2013en_US
dc.identifier.scopusquality--
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.grantfulltextnone-
item.fulltextNo Fulltext-
item.openairetypeConference Object-
item.cerifentitytypePublications-
item.languageiso639-1en-
crisitem.author.dept02.5. Department of Electrical and Electronics Engineering-
Appears in Collections:Elektrik ve Elektronik Mühendisliği Bölümü / Department of Electrical & Electronics Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
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