Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/10379
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dc.contributor.authorKarahan, M.-
dc.contributor.authorKasnakoğlu, C.-
dc.date.accessioned2023-04-16T10:02:10Z-
dc.date.available2023-04-16T10:02:10Z-
dc.date.issued2022-
dc.identifier.isbn9781665453387-
dc.identifier.urihttps://doi.org/10.1109/IC2IE56416.2022.9970136-
dc.identifier.urihttps://hdl.handle.net/20.500.11851/10379-
dc.description5th IEEE International Conference on Computer and Informatics Engineering, IC2IE 2022 -- 13 September 2022 through 14 September 2022 -- 184967en_US
dc.description.abstractDevelopments in information technology have enabled unmanned aerial vehicles to decrease in size, increase their maneuverability and gain vertical landing and take-off features. In this research, a nonlinear model of a quadrotor unmanned aerial vehicle was created using the MATLAB/Simulink program. A robust backstepping controller is designed to provide altitude and attitude control for this model. In order to prove the superiority of the backstepping controller, the results obtained with the classical Proportional Integral Derivative (PID) controller are compared with the performance of the backstepping controller. The rise time, overshoot and settling time values of the PID controller and the backstepping controller were compared. The results showed that the backstepping controller performed more successfully in controlling altitude and attitude angles. © 2022 IEEE.en_US
dc.language.isoenen_US
dc.publisherInstitute of Electrical and Electronics Engineers Inc.en_US
dc.relation.ispartof2022 5th International Conference on Computer and Informatics Engineering, IC2IE 2022en_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectaltitude controlen_US
dc.subjectattitude controlen_US
dc.subjectbackstepping controlen_US
dc.subjectnonlinear systemsen_US
dc.subjectPID controlleren_US
dc.subjectquadrotoren_US
dc.subjectrobust controlen_US
dc.subjectunmanned aerial vehicleen_US
dc.subjectAircraft controlen_US
dc.subjectAltitude controlen_US
dc.subjectAntennasen_US
dc.subjectBacksteppingen_US
dc.subjectControllersen_US
dc.subjectElectric control equipmenten_US
dc.subjectManeuverabilityen_US
dc.subjectMATLABen_US
dc.subjectProportional control systemsen_US
dc.subjectThree term control systemsen_US
dc.subjectTwo term control systemsen_US
dc.subjectUnmanned aerial vehicles (UAV)en_US
dc.subjectAerial vehicleen_US
dc.subjectBackstepping controlen_US
dc.subjectBackstepping controlleren_US
dc.subjectManoeuvrabilityen_US
dc.subjectNon-linear modellingen_US
dc.subjectProportional-integral-derivatives controllersen_US
dc.subjectQuad rotorsen_US
dc.subjectQuadrotor unmanned aerial vehiclesen_US
dc.subjectUnmanned aerial vehicleen_US
dc.subjectVertical landingen_US
dc.subjectRobust controlen_US
dc.titleNonlinear Modeling and Robust Backstepping Control of a Quadrotor Unmanned Aerial Vehicleen_US
dc.typeConference Objecten_US
dc.departmentTOBB ETÜen_US
dc.identifier.startpage94en_US
dc.identifier.endpage99en_US
dc.identifier.scopus2-s2.0-85145358202en_US
dc.institutionauthor…-
dc.identifier.doi10.1109/IC2IE56416.2022.9970136-
dc.authorscopusid57216759940-
dc.authorscopusid24802064500-
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
item.openairetypeConference Object-
item.languageiso639-1en-
item.grantfulltextnone-
item.fulltextNo Fulltext-
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.cerifentitytypePublications-
crisitem.author.dept02.5. Department of Electrical and Electronics Engineering-
Appears in Collections:Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
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