Redesign, analysis, fabrication and testing of light weight wing with solar panels as wing skin for solar UAV : part 1
This report is on the design of a Solar Unmanned Aerial Vehicle (UAV) of mission requirement of Medium Altitude Long Endurance. The report focuses on the airframe configuration and design in the structural aspect of the UAV especially with respect to the wing. The first part of the report covers ana...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2014
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| Online Access: | http://hdl.handle.net/10356/60434 |