Development of solid-state power controller for aerospace applications
There is a developing pattern towards progressively more electric aircraft (MEA) design and system with an expanded number of converters/inverters and electronic circuits. As the electronic system has a favourable position over the conventional mechanical system, the pressure-driven system as far as...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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Nanyang Technological University
2020
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| Online Access: | https://hdl.handle.net/10356/139776 |