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Model-based solutions for structural coupling in flight control systems
Structural Coupling is the interaction between an aircraft's Flight Control System (FCS) and its structural and aero-dynamics. These interactions have the potential to cause significant problems to the aircraft, possibly through structural fatigue failure, or by corruption of sensor readings le...
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| Format: | Default Thesis |
| Published: |
2002
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| Online Access: | https://hdl.handle.net/2134/33748 |
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