摘要
The composite laminate plate contained the piezoelectric patch bonded to surface or embedded was considered. Based on Kirchhoff hypothesis, the finite element model of the plate with induced strain actuators was built. The optimal shape control of the composite plate was studied and the objective function considering shape control and minimum energy consumption was given. The voltage applied to piezoelectric patch was given by using sequence quadratic programming method. The analytical result of the cantilever plate, as an example, was given and the deflection was compared with the experimental results provided by Crawley, E.F..
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 176-179 |
| 页数 | 4 |
| 期刊 | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
| 卷 | 25 |
| 期 | 2 |
| 出版状态 | 已出版 - 1999 |
| 已对外发布 | 是 |
联合国可持续发展目标
此成果有助于实现下列可持续发展目标:
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可持续发展目标 7 经济适用的清洁能源
指纹
探究 'Numerical analysis of optimal control on composite plate deformation' 的科研主题。它们共同构成独一无二的指纹。引用此
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