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Optimization of dynamic behavior of thin-walled laminated cylindrical shells by genetic algorithms and deep neural networks supported by modal shape identification

机译:遗传算法和模态形状识别支持薄壁层压圆柱壳动力学行为的优化

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摘要

This paper presents a novel method for the optimization of the dynamic behavior of a laminated cylinder through stacking sequence optimization. The number of layers reaches 48 and the optimized parameters are either the value of the fundamental natural frequency or the width of the frequency gaps around the excitation force frequencies. The proposed procedure involves automatic mode shape identification and a combined genetic algorithm-deep neural network procedure along with a Curriculum Learning loop, enabling the improvement of accuracy and reduction of computational costs. The proposed optimization algorithm is accurate, robust, and significantly faster than typical genetic algorithm optimization, in which the objective function values are calculated using the finite element method. A rough rule for the estimation of the necessary number of patterns is proposed and the optimal results obtained using the proposed approach are compared to the results obtained using a standard approach (without mode shape identification), in order to demonstrate the effectiveness and robustness of the new method.
机译:本文介绍了通过堆叠序列优化来优化层压圆筒的动态行为的新方法。层数达到48,优化的参数是基本固有频率的值或激发力频率周围的频率间隙的宽度。所提出的程序涉及自动模式形状识别和组合的遗传算法 - 深神经网络过程以及课程学习循环,从而提高了准确性和计算成本的降低。所提出的优化算法比典型的遗传算法优化是准确,稳健的,并且明显快于,其中使用有限元方法计算目标函数值。提出了估计必要数量的图案的粗略规则,并将使用所提出的方法获得的最佳结果与使用标准方法(无模式形状识别)获得的结果进行比较,以证明效果和鲁棒性新方法。

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