Fighter Aircraft Maneuver Limiting Using MPC : Theory and Application
Flight control design for modern fighter aircraft is a challenging task. Aircraft are dynamical systems, which naturally contain a variety of constraints and nonlinearities such as, e.g., maximum permissible load factor, angle of attack and control surface deflections. Taking these limitations into...
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| Format: | Doctoral Thesis |
| Language: | English |
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Linköpings universitet, Reglerteknik
2017
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-139945 http://nbn-resolving.de/urn:isbn:9789176854501 |