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Passive Fault Tolerant Lateral Controller Design For an UAV

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dc.contributor.authorVural, Sitki Yenal
dc.contributor.authorDasdemir, Janset
dc.contributor.authorHajiyev, Chingiz
dc.date.accessioned2026-06-27T14:14:25Z
dc.date.issued2018
dc.description.abstractIn this study a passive lateral fault tolerant controller for an UAV is designed using dynamic inversion (DI) method and robust integral of the signum of the error (RISE) techniques. The details of the methods are summarized As the reference model of the tracking controller, UAV controlled by feedback type controller is used and the control method used for this design is explained. The loss in control effectiveness is modeled as changes in the control distribution matrix. Simulations are made to show the effectiveness of the passive fault tolerant controller in maintaining the lateral control in case of actuator effectiveness loss. (C) 2018, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.en
dc.description.urihttps://doi.org/10.1016/j.ifacol.2018.11.320
dc.identifier.doi10.1016/j.ifacol.2018.11.320
dc.identifier.endpage451
dc.identifier.issn2405-8963
dc.identifier.issue30
dc.identifier.startpage446
dc.identifier.urihttps://hdl.handle.net/20.500.14981/58328
dc.identifier.volume51
dc.identifier.wos000451096700085
dc.language.isoeng
dc.publisherELSEVIER
dc.relation.conference18th International-Federation-of-Automatic-Control (IFAC) Conference on Technology, Culture and International Stability (TECIS)
dc.relation.ispartofIFAC PAPERSONLINE
dc.rightsopenAccess
dc.subjectFault-tolerant control
dc.subjectUAVs
dc.subjectRobust control
dc.subjectUAV control
dc.subjectActuator failure
dc.subjectAutomation & Control Systems
dc.titlePassive Fault Tolerant Lateral Controller Design For an UAV
dc.typeProceedings Paper
dspace.entity.typePublication
local.import.sourceWOS

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