File Download

There are no files associated with this item.

  • Find it @ UNIST can give you direct access to the published full text of this article. (UNISTARs only)
Related Researcher

오현동

Oh, Hyondong
Autonomous Systems Lab.
Read More

Views & Downloads

Detailed Information

Cited time in webofscience Cited time in scopus
Metadata Downloads

Full metadata record

DC Field Value Language
dc.citation.endPage 7343 -
dc.citation.number 15 -
dc.citation.startPage 7317 -
dc.citation.title INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL -
dc.citation.volume 31 -
dc.contributor.author Ngo Phong Nguyen -
dc.contributor.author Oh, Hyondong -
dc.contributor.author Kim, Yoonsoo -
dc.contributor.author Moon, Jun -
dc.contributor.author Yang, Jun -
dc.contributor.author Chen, Wen-Hua -
dc.date.accessioned 2023-12-21T15:12:45Z -
dc.date.available 2023-12-21T15:12:45Z -
dc.date.created 2021-07-23 -
dc.date.issued 2021-10 -
dc.description.abstract This article proposes a finite-time disturbance observer-based modified super-twisting algorithm (FDO-STA) for disturbed high-order integrator-chain systems under matched and mismatched disturbances. We first design a finite-time observer for disturbance estimation, in which we show the finite-time convergence of disturbance estimation errors to zero. Second, by employing the estimates of disturbances and their derivatives, a new dynamic sliding surface is derived, which ensures the finite-time convergence of the controlled output to zero in the sliding phase. Then, based on the estimates of disturbances and their derivatives, the designed sliding surface, and a modified super-twisting algorithm, we develop the FDO-STA, which guarantees the finite-time convergence of the sliding variable to zero in the reaching phase. Rigorous analysis is provided to show the finite-time stability of the overall closed-loop system under the proposed control scheme. We finally apply the proposed FDO-STA framework to the path following control for fixed-wing UAVs under wind disturbances. Various simulation results are provided to show the effectiveness of the proposed controller, compared with the existing control approaches. -
dc.identifier.bibliographicCitation INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, v.31, no.15, pp.7317 - 7343 -
dc.identifier.doi 10.1002/rnc.5678 -
dc.identifier.issn 1049-8923 -
dc.identifier.scopusid 2-s2.0-85109160748 -
dc.identifier.uri https://scholarworks.unist.ac.kr/handle/201301/53308 -
dc.identifier.url https://onlinelibrary.wiley.com/doi/10.1002/rnc.5678 -
dc.identifier.wosid 000670280700001 -
dc.language 영어 -
dc.publisher WILEY -
dc.title Finite-time disturbance observer-based modified super-twisting algorithm for systems with mismatched disturbances: Application to fixed-wing UAVs under wind disturbances -
dc.type Article -
dc.description.isOpenAccess FALSE -
dc.relation.journalWebOfScienceCategory Automation & Control Systems; Engineering, Electrical & Electronic; Mathematics, Applied -
dc.relation.journalResearchArea Automation & Control Systems; Engineering; Mathematics -
dc.type.docType Article; Early Access -
dc.description.journalRegisteredClass scie -
dc.description.journalRegisteredClass scopus -
dc.subject.keywordAuthor finite-time disturbance observer -
dc.subject.keywordAuthor fixed-wing UAVs -
dc.subject.keywordAuthor matched and mismatched disturbances -
dc.subject.keywordAuthor modified super-twisting algorithm -
dc.subject.keywordAuthor path following control -
dc.subject.keywordPlus SLIDING-MODE CONTROL -
dc.subject.keywordPlus PATH-FOLLOWING CONTROL -
dc.subject.keywordPlus ATTITUDE STABILIZATION -
dc.subject.keywordPlus UNCERTAIN SYSTEMS -
dc.subject.keywordPlus OUTPUT REGULATION -
dc.subject.keywordPlus SURFACE DESIGN -
dc.subject.keywordPlus SPACECRAFT -

qrcode

Items in Repository are protected by copyright, with all rights reserved, unless otherwise indicated.