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Altitude control of a quadcopter using interval type-2 fuzzy controller with dynamic footprint of uncertainty

dc.contributor.authorSahin, Ihsan
dc.contributor.authorUlu, Cenk
dc.date.accessioned2026-06-27T14:48:05Z
dc.date.issued2023
dc.description.abstractFootprint of uncertainty (FOU) characteristics of interval type-2 membership functions (IT2-MFs) play an important role in the performance and robustness of interval type-2 fuzzy controllers (IT2-FCs). In literature, fixed FOU structures are used in almost all IT2-FC designs. In this study, an IT2-FC with dynamic FOU is proposed to provide high performance and robustness in the altitude control of a quadcopter. A proportional-derivative (PD) type FC with Takagi-Sugeno rule structure is used in the design procedure of the proposed controller. Additionally, input variables (error and derivative of error) are defined by using triangular IT2-MFs. To provide a dynamic FOU structure, the height of the lower MF (LMF) of each interval type-2 fuzzy set is defined as a function of the system error. In this way, FOU levels of IT2-MFs are adjusted dynamically since the height value of the LMF directly determines the FOU level of the IT2-MF. To evaluate the effectiveness of the proposed controller, comparison studies are performed under different conditions, including unmodeled measurement noises, an external disturbance, and a system parameter uncertainty. A classical PD, a type-1 fuzzy PD, and an interval type-2 fuzzy PD with fixed FOU controllers are used in the comparisons. The comparison results demonstrate that the proposed interval type-2 fuzzy PD controller with dynamic FOU exhibits better performance and more robustness than the other controllers.(c) 2022 ISA. Published by Elsevier Ltd. All rights reserved.en
dc.description.urihttps://doi.org/10.1016/j.isatra.2022.08.020
dc.identifier.doi10.1016/j.isatra.2022.08.020
dc.identifier.eissn1879-2022
dc.identifier.endpage94
dc.identifier.issn0019-0578
dc.identifier.pubmed36088131
dc.identifier.startpage86
dc.identifier.urihttps://hdl.handle.net/20.500.14981/64941
dc.identifier.volume134
dc.identifier.wos000956273500001
dc.language.isoeng
dc.publisherELSEVIER SCIENCE INC
dc.relation.ispartofISA TRANSACTIONS
dc.subjectQuadcopter
dc.subjectAltitude control
dc.subjectType-2 fuzzy logic controller
dc.subjectFootprint of uncertainty
dc.subjectRobustness
dc.subjectPD controller
dc.subjectLOGIC SYSTEMS
dc.subjectPERFORMANCE
dc.subjectDESIGN
dc.subjectMODEL
dc.subjectPI
dc.subjectTRACKING
dc.subjectATTITUDE
dc.subjectAutomation & Control Systems
dc.subjectEngineering
dc.subjectInstruments & Instrumentation
dc.titleAltitude control of a quadcopter using interval type-2 fuzzy controller with dynamic footprint of uncertainty
dc.typeArticle
dspace.entity.typePublication
local.import.sourceWOS

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