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College of Engineering/Engineering Practice School (공과대학/대학원)
Dept. of Mechanical Aerospace Engineering (기계항공공학부)
Others_기계항공공학부
6절 링크 방식의 날갯짓 초소형 비행체 설계 및 실험 : Experimental Study on a Flapping-Wing Micro Air Vehicle Using a Six-Bar Linkage
- Authors
- Issue Date
- 2016-03-10
- Publisher
- 제어로봇시스템학회
- Citation
- 2016 제31회 제어로봇시스템학회 학술대회, pp. 15-16
- Keywords
- 6절 링크 방식의 날갯짓 초소형 비행체 설계 및 실험 ; 공학 ; flapping wing ; MAV
- Abstract
- This 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.
- Language
- Korean
- Files in This Item:
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