Control system design and aggressive maneuver method for a quad-rotor UAV쿼드-로터 무인항공기의 제어시스템 설계 및 고기동 기법 연구

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dc.contributor.advisorTahk, Min-Jea-
dc.contributor.advisor탁민제-
dc.contributor.authorLee, Byung-Yoon-
dc.contributor.author이병윤-
dc.date.accessioned2013-09-11-
dc.date.available2013-09-11-
dc.date.issued2013-
dc.identifier.urihttp://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=515213&flag=dissertation-
dc.identifier.urihttp://hdl.handle.net/10203/179664-
dc.description학위논문(석사) - 한국과학기술원 : 항공우주공학전공, 2013.2, [ vi, 44 p. ]-
dc.description.abstractThis thesis focuses on dynamic modeling, control system design and aggressive maneuver method for a Quad-rotor UAV. Quad-rotor UAV is modeled by 6-DOF nonlinear equations of motion. We introduce flip maneuver for a Quad-rotor UAV and design control method. Three attitude controllers of the Quad-rotor are designed by various methodologies for performing aggressive maneuver such as flip maneuver. Performances of these controllers are compared using 6-DOF simulation results. We built Quad-rotor platform and performed flight test to show the possibility of the real-world flip maneuver of a Quad-rotor.eng
dc.languageeng-
dc.publisher한국과학기술원-
dc.subjectQuad-rotor-
dc.subjectAggressive Maneuver-
dc.subjectOpen-loop Control-
dc.subject쿼드-로터-
dc.subject고기동-
dc.subject개루프 제어-
dc.subject슬라이딩 모드 제어-
dc.subjectSliding Mode Control-
dc.titleControl system design and aggressive maneuver method for a quad-rotor UAV-
dc.title.alternative쿼드-로터 무인항공기의 제어시스템 설계 및 고기동 기법 연구-
dc.typeThesis(Master)-
dc.identifier.CNRN515213/325007 -
dc.description.department한국과학기술원 : 항공우주공학전공, -
dc.identifier.uid020113423-
dc.contributor.localauthorTahk, Min-Jea-
dc.contributor.localauthor탁민제-
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AE-Theses_Master(석사논문)
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