Development of flight test platform for flapping wings micro air vehicles

Development of flight test platform for flapping wings micro air vehicles

This report presents the design, fabrication process, analysis and characterization of simple and low cost test platforms for force measurement of Flapping Wing Micro Air Vehicles (FWMAVs). Simple pendulum method and linearly guided load cell based test platforms currently used by the research group...

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Bibliographic Details
Main Author: Pradipta, Johanes Eldwin
Other Authors: Lau Gih Keong
Format: Final Year Project (FYP)
Language:English
Published: 2015
Subjects:
DRNTU::Engineering::Mechanical engineering::Machine design and construction
Online Access:http://hdl.handle.net/10356/64582

Internet

http://hdl.handle.net/10356/64582

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