Integrated structural design, vibration control, and aeroelastic tailoring by multiobjective optimization
The integrated design of a structure and its control system was treated as a multiobjective optimization problem. Structural mass, a quadratic performance index, and the flutter speed constituted the vector objective function. The closed-loop performance index was taken as the time integral of th...
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| Format: | Others |
| Language: | en |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/38912 http://scholar.lib.vt.edu/theses/available/etd-07282008-134827/ |