Aircraft wing flutter control
This research includes the design of a multivariable control system for aircraft wings. Two objectives are desired. The first is to control the vibrational problem for low-speed flight by applying a feedback control strategy. The second goal is to demonstrate that the controller for this wing assemb...
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| Main Author: | Tavalla, Sahar Sadat (author) |
|---|---|
| Published: |
2013
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| Subjects: | |
| Online Access: | http://bspace.buid.ac.ae/handle/1234/392 |
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