In this paper, for the first time active vibration control of rotating laminated composite truncated conical shells containing magnetostrictive layers by employing first-order shear deformation theory is investigated. The active vibration control task is done through magnetostrictive layers employing velocity feedback control law. The effects of initial hoop tension and centrifugal and Coriolis forces are considered in extraction of the partial differential equations through Hamilton principle. The ordinary differential equations are derived by employing modified Galerkin method. This study agrees with the mentioned results of the literature. Finally, the effects of several parameters on the vibration suppression are investigated.

本文采用一阶剪切变形理论，首次研究了旋转旋转的包含磁致伸缩层的复合材料截顶圆锥壳的主动振动控制。主动振动控制任务是通过采用速度反馈控制律的磁致伸缩层来完成的。通过汉密尔顿原理提取偏微分方程时，考虑了初始环向张力，离心力和科里奥利力的影响。利用改进的Galerkin方法推导了常微分方程。这项研究与文献中提到的结果一致。最后，研究了几个参数对减振的影响。