Performance comparison of three different types of attitude control systems of the quad-rotor UAV to perform flip maneuver

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dc.contributor.authorLee, Byung Yoonko
dc.contributor.authorYoo, Dong Wanko
dc.contributor.authorTahk, Min-Jeako
dc.date.accessioned2014-08-28-
dc.date.available2014-08-28-
dc.date.created2014-02-05-
dc.date.created2014-02-05-
dc.date.created2014-02-05-
dc.date.issued2013-03-
dc.identifier.citationINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.14, no.1, pp.58 - 66-
dc.identifier.issn2093-274X-
dc.identifier.urihttp://hdl.handle.net/10203/187448-
dc.description.abstractThis paper addresses the performance of three different types of attitude control systems for the Quad-rotor UAV to perform the flip maneuver. For this purpose, Quad-rotor UAV's 6-DOF dynamic model is derived, and it was used for designing an attitude controller of the Quad-rotor UAV. Attitude controllers are designed by three different methods. One is the open-loop control system design, another is the PD control system design, and the last method is the sliding mode control system design. Performances of all controllers are tested by 6-DOF simulation. In case of the open-loop control system, control inputs are calculated by the quad-rotor dynamic model and thrust system model that are identified by the thrust test. The 6-DOF real- time simulation environment was constructed in order to verify the performances of attitude controllers.-
dc.languageEnglish-
dc.publisherThe Korean Society for Aeronautical & Space Sciences-
dc.titlePerformance comparison of three different types of attitude control systems of the quad-rotor UAV to perform flip maneuver-
dc.typeArticle-
dc.identifier.wosid000346989800006-
dc.identifier.scopusid2-s2.0-84875892544-
dc.type.rimsART-
dc.citation.volume14-
dc.citation.issue1-
dc.citation.beginningpage58-
dc.citation.endingpage66-
dc.citation.publicationnameINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES-
dc.identifier.doi10.5139/IJASS.2013.14.1.58-
dc.contributor.localauthorTahk, Min-Jea-
dc.description.isOpenAccessN-
dc.type.journalArticleArticle-
dc.subject.keywordAuthor6-DOF real-time simulation-
dc.subject.keywordAuthorFlip maneuver-
dc.subject.keywordAuthorOpen-loop control-
dc.subject.keywordAuthorQuad-rotor UAV-
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AE-Journal Papers(저널논문)
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