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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Bibliographic Details
Main Author: Tavalla, Sahar Sadat (author)
Published: 2013
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Online Access:http://bspace.buid.ac.ae/handle/1234/392
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