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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| 格式: | Theses and Dissertations |
| 語言: | English |
| 出版: |
2013
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| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/55146 |
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| 機構: | Nanyang Technological University |
| 語言: | English |