DC Field | Value | Language |
---|---|---|
dc.contributor.advisor | Tahk, Min-Jea | - |
dc.contributor.advisor | 탁민제 | - |
dc.contributor.author | Lee, Byung-Yoon | - |
dc.contributor.author | 이병윤 | - |
dc.date.accessioned | 2013-09-11 | - |
dc.date.available | 2013-09-11 | - |
dc.date.issued | 2013 | - |
dc.identifier.uri | http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=515213&flag=dissertation | - |
dc.identifier.uri | http://hdl.handle.net/10203/179664 | - |
dc.description | 학위논문(석사) - 한국과학기술원 : 항공우주공학전공, 2013.2, [ vi, 44 p. ] | - |
dc.description.abstract | This 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.language | eng | - |
dc.publisher | 한국과학기술원 | - |
dc.subject | Quad-rotor | - |
dc.subject | Aggressive Maneuver | - |
dc.subject | Open-loop Control | - |
dc.subject | 쿼드-로터 | - |
dc.subject | 고기동 | - |
dc.subject | 개루프 제어 | - |
dc.subject | 슬라이딩 모드 제어 | - |
dc.subject | Sliding Mode Control | - |
dc.title | Control system design and aggressive maneuver method for a quad-rotor UAV | - |
dc.title.alternative | 쿼드-로터 무인항공기의 제어시스템 설계 및 고기동 기법 연구 | - |
dc.type | Thesis(Master) | - |
dc.identifier.CNRN | 515213/325007 | - |
dc.description.department | 한국과학기술원 : 항공우주공학전공, | - |
dc.identifier.uid | 020113423 | - |
dc.contributor.localauthor | Tahk, Min-Jea | - |
dc.contributor.localauthor | 탁민제 | - |
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