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The Effect of Folding on Motion Flapping Wing Aero Vehicle
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Title
The Effect of Folding on Motion Flapping Wing Aero Vehicle
Issued Date
2017-11-16
Citation
Kim, Do-Young. (2017-11-16). The Effect of Folding on Motion Flapping Wing Aero Vehicle. IEEE International Conference on Multisensor Fusion and Integration for Intelligent Systems, MFI 2017, 597–601. doi: 10.1109/MFI.2017.8170387
Type
Conference Paper
ISBN
9781509060641
Abstract
An interesting about MAV and a research for flapping wing aero vehicle has been increased. It is required that take-off and landing abilities to lift up a vehicle by flapping motion to achieve a special purpose for flapping wing aero vehicle. An airfoil has to generate lift force more than a weight of the body to work take-off from the ground without additional force. MAV can generate enough lift force, abilities of MAV: load capacity, reliability, damage reduction. In this study, we propose a four-bar linkage structure to generate lift force. And an experiment will be set up to measure the lift force with a folding mechanism of flapping wing. After this, the result will be used for development of nature-inspired bird robot. © 2017 IEEE.
URI
http://hdl.handle.net/20.500.11750/47041
DOI
10.1109/MFI.2017.8170387
Publisher
IEEE Robotics and Automation Society (RAS), IEEE Industrial Electronics Society (IES)
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윤동원
Yun, Dongwon윤동원

Department of Robotics and Mechatronics Engineering

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