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6절 링크 방식의 날갯짓 초소형 비행체 설계 및 실험 : Experimental Study on a Flapping-Wing Micro Air Vehicle Using a Six-Bar Linkage

DC Field Value Language
dc.contributor.author이준희en
dc.contributor.author김영환-
dc.contributor.author전재혁-
dc.contributor.author신상준-
dc.contributor.author김종암-
dc.creator김종암-
dc.date.accessioned2017-10-23T06:47:35Z-
dc.date.available2017-12-22T14:43:54Z-
dc.date.issued2016-03-10-
dc.identifier.citation2016 제31회 제어로봇시스템학회 학술대회, pp. 15-16-
dc.identifier.urihttps://hdl.handle.net/10371/135235-
dc.description.abstractThis paper presents an experimental study on a Flapping-Wing Micro Air Vehicle (FWMAV) using a six-bar linkage mechanism. To design the mechanism, a conceptual design process was employed, and then the design was analyzed using a multi-body dynamic program. The designed FWMAV was manufactured and verified by a high-speed camera and a six-force external balance. As a result, the FWMAVs aerodynamic performances such as thrust and moments were confirmed through the experiment.-
dc.language.isoko-
dc.publisher제어로봇시스템학회en
dc.subject6절 링크 방식의 날갯짓 초소형 비행체 설계 및 실험en
dc.subject공학en
dc.subjectflapping wing-
dc.subjectMAV-
dc.title6절 링크 방식의 날갯짓 초소형 비행체 설계 및 실험en
dc.title.alternativeExperimental Study on a Flapping-Wing Micro Air Vehicle Using a Six-Bar Linkage-
dc.typeConference Paper-
dc.description.srndOAIID:RECH_ACHV_DSTSH_NO:A201625932-
dc.description.srndRECH_ACHV_FG:RR00200003-
dc.description.srndADJUST_YN:-
dc.description.srndEMP_ID:A001138-
dc.description.srndCITE_RATE:-
dc.description.srndFILENAME:6_절_링크_방식의_날갯짓_초소형_비행체_설계_및_실험.pdf-
dc.description.srndDEPT_NM:기계항공공학부-
dc.description.srndEMAIL:chongam@snu.ac.kr-
dc.description.srndSCOPUS_YN:-
dc.description.srndFILEURL:https://srnd.snu.ac.kr/eXrepEIR/fws/file/414326ff-e8ee-4e2a-a0bf-9bae95b095d6/link-
dc.description.srndCONFIRM:Y-
dc.identifier.srndA201625932-
Appears in Collections:
College of Engineering/Engineering Practice School (공과대학/대학원)Dept. of Mechanical Aerospace Engineering (기계항공공학부)Others_기계항공공학부
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