Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams

Publisher： Trans Tech Publications

E-ISSN： 1662-7482|2015|798|292-296

ISSN： 1660-9336

Source： Applied Mechanics and Materials, Vol.2015, Iss.798, 2015-11, pp. : 292-296

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