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Active vibration control of complex structures in modal space
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Date
2014
Author
Mersin, Kemal
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Aerospace structures are designed to be light-weight to obtain high performance. Reduction in weight makes the structure flexible and lower frequency modes can be easily excited. Moreover those modes have low damping and vibrations do not attenuate immediately. Passive systems are effective to control the vibrations but they can be heavy and most of the time they do not respond to changing environment conditions. An active system is necessary for low-weight adaptive vibration reduction system. Modal Space Control is used for large flexible aerospace structures due to the advantage of reducing the complexity of control system. In this study a generalized formulation of modal space control is proposed for three dimensions where each node is modeled with six degrees of freedom.
Subject Keywords
Air-to-air missiles
,
Guided missiles
,
Guidance systems (Flight).
URI
http://etd.lib.metu.edu.tr/upload/12618264/index.pdf
https://hdl.handle.net/11511/24271
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Graduate School of Natural and Applied Sciences, Thesis
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K. Mersin, “Active vibration control of complex structures in modal space,” M.S. - Master of Science, Middle East Technical University, 2014.
