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摘要

抛物面旋转壳体常用于通信系统、精密光机械系统和航空航天结构中。本文研究了带有分段作动器贴片的抛物面壳层合的精密分布控制效果。首先给出了受机械力、温度力和控制力影响的分布驱动层叠合的抛物面壳的数学模型,然后使用假设的模态振型函数给出了分布控制力及其贡献的子向/周向膜和弯曲控制元件的公式。研究了抛物壳的致动器位置、控制力、贡献分量和归一化控制权限。这些力和膜/弯曲分量基本上表现出不同的模态特征,受壳体几何形状和其他设计参数的影响。分析表明,膜贡献成分主导了整体控制效果。归一化力较大的位置表示控制效率较高的区域,即单位致动器区域的诱导控制力较大。在执行器有限的情况下,将执行器放置在这些位置将产生最大的控制效果。
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Actuator Placement and Control Efficiency of Paraboloidal Shell Structures
Paraboloidal shells of revolution are commonly used in communication systems, precision opto-mechanical systems and aerospace structures. This study is to investigate the precision distributed control effectiveness of paraboloidal shells laminated with segmented actuator patches. Mathematical models of the paraboloidal shells laminated with distributed actuator layers subjected to mechanical, temperature, and control forces are presented first, followed by formulations of distributed control forces with their contributing meridional/circumferential membrane and bending control components using an assumed mode shape function. Studies of actuator placements, control forces, contributing components, and normalized control authorities of paraboloidal shells are carried out. These forces and membrane/bending components basically exhibit distinct modal characteristics influenced by shell geometries and other design parameters. Analyses suggest that the membrane contributed components dominate the overall control effect. Locations with larger normalized forces indicate the areas with high control efficiencies, i.e., larger induced control force per unit actuator area. With limited actuators, placing actuators at those locations would lead to the maximal control effects.
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