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Fuzzy frequency response estimation from experimental data: Definition and application in mechanical structures of aircraft and aerospace vehicles

机译:实验数据的模糊频率响应估计:飞机和航空航天器机械结构的定义和应用

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Fuzzy frequency response estimation from experimental data: definition and application in mechanical structures of aircraft and aerospace vehicles is proposed in this paper. A fuzzy c-Means clustering algorithm is used to organize the input and output experimental data of a free free aluminium beam into groups based on similarities among the data. Starting from the fuzzy clustering a methodology for identification of the linear sub-models, in terms of transfer function, that represent the free free aluminium beam in operation regions is developed and these linear sub-models are organized according to Takagi-Sugeno (TS) fuzzy representation. A fuzzy frequency estimation of the aluminium beam is determined through the frequency response function. The main contribution of this paper is to demonstrate through the proposal of a Theorem, that fuzzy frequency response estimation is a boundary in the magnitude and phase Bode plots. Studies on the aluminum beam are used for analysis and control of vibration in mechanical structures of aircraft and aerospace vehicles.
机译:从实验数据估计模糊频率响应:本文提出了在飞机和航空航天器的机械结构的定义和应用。基于数据之间的相似性,使用模糊c均值聚类算法将自由的自由铝梁的输入和输出实验数据组织为组。从模糊聚类开始,开发了一种基于传递函数的线性子模型识别方法,该模型表示操作区域中的自由自由铝梁,并且根据Takagi-Sugeno(TS)来组织这些线性子模型模糊表示。通过频率响应函数确定铝梁的模糊频率估计。本文的主要贡献是通过一个定理的建议来证明模糊频率响应估计是幅值和相位波特图的边界。对铝梁的研究被用于分析和控制飞机和航空航天器的机械结构中的振动。

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