Piezoelectric intelligent structures have been widely applied in aerospace engineering.
压电智能结构在航天、航空工程获得了广泛应用。
The finite element dynamic model for intelligent structures is formulated with a new piezoelectric plate bending element in this paper.
采用一种新的压电板单元，建立了含有分布压电传感元件和执行元件结构（智能结构）的有限元动力模型。
Active vibration control for piezoelectric intelligent structures is an important task in the field of engineering structural research.
随机压电智能结构振动主动控制是目前结构动力设计与控制研究领域中的一个重要的崭新课题。
Hamilton's principle is used to derive the equation of piezoelectric thin films and the dynamic finite element equations of intelligent structures.
利用哈密顿原理推导出压电结构的变分方程，建立了智能结构的有限元动力方程。
The experiment of intelligent structures has been studied, and the new control law and optimal configure rule have been validated through the experiment results.
通过对压电智能结构实验进行分析，所得到的实验结果验证了控制律算法和驱动器位置优化配置方法的正确性和优越性。
The piezoelectric materials have strong electromechanical couple ability so that they are mostly used in intelligent structures especially for the problem of vibration control.
压电材料(压电陶瓷和压电聚合物)具有很强的力电耦合效应而成为智能结构中应用最为广泛的智能材料。
The dynamic models of a specific precise instrument in spacecraft are established and an active vibration isolation system based on piezoelectric intelligent structures is constructed.
对某特定的机载精密仪器进行了动力学建模，建立了压电智能结构主动隔振系统。
Intelligent structures are being the focus in the study of vibration control because of it's advantages of fast reaction self-adapting self-diagnosing and self-recovery.
智能结构由于具有响应快、自适应、自诊断、自修复之优点逐渐成为振动控制领域里研究的热点。
The optical fiber system embedded in composite materials will become a "Neutral Network System" of the future aircraft structures, leading to new concepts of the "Intelligent Structures".
提出了埋设于复合材料内部的光纤系统将成为未来飞行器结构的“神经网络系统”而使结构成为“智能结构”等新概念。
The optical fiber system embedded in composite materials will become a "Neutral Network System" of the future aircraft structures, leading to new concepts of the "Intelligent Structures".
提出了埋设于复合材料内部的光纤系统将成为未来飞行器结构的“神经网络系统”而使结构成为“智能结构”等新概念。
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