Controllability of morphing wing of UAV using shape memory alloy
The aim of this project is to study the controllability of a morphing UAV wing flap, actuated by shape memory alloy wires. The morphing wing flap prototype was fabricated by Thomas. In this project, the prototype response with SM495 0.185 mm dia NiTi wire. The wing flap is actuated using SMA, which...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2009
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| Online Access: | http://hdl.handle.net/10356/17186 |