Perching aircraft dynamics and control optimization
This final year project covers the optimization of aircraft perching maneuver through geometric reconfiguration or morphing. A novel Unmanned Aerial Vehicle (UAV) model which adopts canard configuration and variable-incidence outer wings is specially designed for the analysis of perching maneuver. A...
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| 主要作者: | |
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| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
2009
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| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/16202 |
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| 機構: | Nanyang Technological University |
| 語言: | English |