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Mathematical modelling of aircraft electrical power systems
The continuing developments in aircraft electrical power supply systems have been accompanied by a progressive narrowing of the transient and the steagy-state voltage regulation limits within which the system must operate. The performance of a system is satisfactory only when it meets the conditions...
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| Format: | Default Thesis |
| Published: |
1981
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| Online Access: | https://hdl.handle.net/2134/13859 |
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