Publications
Detailed Information
Aerodynamic Design and Experiment for Flapping-Wing Micro Air Vehicle Using a Six-Bar Linkage : 6절링크를 이용한 날갯짓 초소형 비행체 공력 설계 및 실험
Cited 0 time in
Web of Science
Cited 0 time in Scopus
- Authors
- Advisor
- 김종암
- Major
- 공과대학 기계항공공학부
- Issue Date
- 2016-02
- Publisher
- 서울대학교 대학원
- Keywords
- flapping-wing ; MAV ; six-bar linkage ; wing trajectory ; multi-bodi dynamics
- Description
- 학위논문 (석사)-- 서울대학교 대학원 : 기계항공공학부, 2016. 2. 김종암.
- Abstract
- The following study demonstrates the design and experimental results of the insect-mimicking Flapping-Wing Micro Air Vehicle (FWMAV) mechanism utilizing a six-bar linkage. The designed vehicle has the distinctive ability to tightly maneuver in limited spaces through only a small alteration in the location of the joint connecting the linkage's end and the fuselage, which in turn radically changes the wing trajectory. We mapped this wing trajectory in order to implement the concept of fully-controlled the FWMAV using Recurdyn
a multibody dynamics software. Upon research of the wing trajectory, the concept of fully controlling the FWMAV was solidified. The multi-body dynamic analysis allowed us to predict the amount of stress existing in each link prior to fabrication, enabling the construction of a more reliable component. As a result, possible operational errors during the production process were minimized. A test-bed was constructed to validate the assembled FWMAVs performance, where the FWMAVs aerodynamic forces and moments were confirmed through the experiment and generated sufficient vertical force to carry out guided flight test.
- Language
- English
- Files in This Item:
Item View & Download Count
Items in S-Space are protected by copyright, with all rights reserved, unless otherwise indicated.