Design and testing of a solid-state power controller control and protection card for aerospace application
Advancements in the field of electrical and electronic aircraft technologies have introduced a concept of a ‘More Electric Aircraft’. This concept essentially replaces non-electrical systems on an aircraft such as Hydraulic and Pneumatic systems with electrical systems. This will create an environme...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2019
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| Online Access: | http://hdl.handle.net/10356/78355 |