Altitude control of quadcopter with symbolic limited optimal discrete control

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dc.contributor.authorÖzbaltan M.
dc.contributor.authorÇaşka S.
dc.date.accessioned2024-07-22T08:01:20Z
dc.date.available2024-07-22T08:01:20Z
dc.date.issued2024
dc.description.abstractIn recent years, quadcopter UAVs have been extensively utilized. Controlling quadcopters is a major concern, and researchers are actively studying it. In this study, altitude control of a quadcopter UAV is achieved using the symbolic limited optimal discrete controller synthesis technique. The resulting controller is compared with the adaptive PID control method, where the PID controller’s parameters are determined using the Dragonfly algorithm. The findings show the superior performance of our approach. © The Author(s), under exclusive licence to Springer-Verlag GmbH Germany, part of Springer Nature 2023.
dc.identifier.DOI-ID10.1007/s40435-023-01278-3
dc.identifier.issn2195268X
dc.identifier.urihttp://akademikarsiv.cbu.edu.tr:4000/handle/123456789/11390
dc.language.isoEnglish
dc.publisherSpringer Science and Business Media Deutschland GmbH
dc.subjectControllers
dc.subjectElectric control equipment
dc.subjectProportional control systems
dc.subjectScattering parameters
dc.subjectThree term control systems
dc.subjectAdaptive PID
dc.subjectControl methods
dc.subjectDiscrete Control
dc.subjectDiscrete controller synthesis
dc.subjectDragonfly algorithm
dc.subjectPID controllers
dc.subjectQuadcopter
dc.subjectS -parameters
dc.subjectSymbolic limited optimal discrete control
dc.subjectSynthesis techniques
dc.subjectAltitude control
dc.titleAltitude control of quadcopter with symbolic limited optimal discrete control
dc.typeArticle

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