Piezo smart composite wing with LQG/LTR control


The objective of the present work is the investigating of the capabilities of piezoelectric actuators as active vibration control devices for wing structures. The first step of the study is that of providing the basic order two structural equation of the system by an ANSYS FEM structural modelling, as it was proceeded in recent works of the authors. The… (More)


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@article{Munteanu2008PiezoSC, title={Piezo smart composite wing with LQG/LTR control}, author={Eliza Munteanu and Ioana Ursu}, journal={2008 IEEE International Symposium on Industrial Electronics}, year={2008}, pages={1160-1165} }