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Decentralized Formation Flight via PID and Integral Sliding Mode Control

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dc.contributor.authorThien, R.T.Y.-
dc.contributor.authorKim, Y.-
dc.date.accessioned2022-12-26T18:04:20Z-
dc.date.available2022-12-26T18:04:20Z-
dc.date.issued2018-
dc.identifier.issn2405-8963-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/13044-
dc.description.abstractThis paper solves a formation control problem for a group of vehicles such as UAVs on a directed network subject to constant and time-varying disturbances or commands. A celebrated PID control is first proposed for constant disturbance rejection then, integral sliding mode control is introduced to tackle unknown but bounded time-varying disturbances or commands. In addition, the control sensitivity with respect to the network topology is analyzed. Finally, a quadcopter formation platform is introduced and used to verify all the presented theoretical results experimentally. ? 2018-
dc.format.extent3-
dc.language영어-
dc.language.isoENG-
dc.publisherElsevier B.V.-
dc.titleDecentralized Formation Flight via PID and Integral Sliding Mode Control-
dc.typeArticle-
dc.publisher.location네델란드-
dc.identifier.doi10.1016/j.ifacol.2018.12.003-
dc.identifier.scopusid2-s2.0-85058476608-
dc.identifier.bibliographicCitationIFAC-PapersOnLine, v.51, no.23, pp 13 - 15-
dc.citation.titleIFAC-PapersOnLine-
dc.citation.volume51-
dc.citation.number23-
dc.citation.startPage13-
dc.citation.endPage15-
dc.type.docTypeConference Paper-
dc.description.isOpenAccessY-
dc.description.journalRegisteredClassscopus-
dc.subject.keywordAuthorFormation control-
dc.subject.keywordAuthorintegral sliding mode control-
dc.subject.keywordAuthormulti-agent system-
dc.subject.keywordAuthorPID control-
dc.subject.keywordAuthortime-varying disturbance-
dc.subject.keywordAuthorunmanned aerial vehicle (UAV)-
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