Solar UAV : design and fabrication of structural test rig for loading and testing a 7.5m half wing
The Solar UAV is a multi-functional aerial vehicle that can be used in many applications. The objective of the project was to design and manufacture a Solar UAV with wingspan of 17.5m, take-off weight of 60kg and having an endurance of 24 hours. To achieve this feat, a lightweight design...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2013
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| Online Access: | http://hdl.handle.net/10356/54145 |