Effective optimal control of a fighter aircraft engine
Typical modem fighter aircraft use two-spool, low by-pass ratio, turbojet engines to provide the thrust needed to carry out the combat manoeuvres required by present-day air warfare tactics. The dynamic characteristics of such aircraft engines are complex and non-linear. The need for fast, accurate...
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| Format: | Default Thesis |
| Published: |
1988
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| Online Access: | https://hdl.handle.net/2134/7287 |
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