Optimizing flexible wing composite structure for mini-uavs

Unmanned Aerial Vehicles [UAV] are famous in modem Civil and military aerospace applications. Its functionality and size lie in a broad area from small spy UAV to drone attack UAV and various civil applications like traffic observation and reporting. Mini Unmanned Aerial Vehicle abbreviated as...

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Bibliographic Details
Main Author: Weerasooriya Mudiyanselage.
Other Authors: Sunil Chandrakant Joshi
Format: Theses and Dissertations
Language:English
Published: 2013
Subjects:
Online Access:http://hdl.handle.net/10356/55146
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Institution: Nanyang Technological University
Language: English
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