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基于神经网络的替代模型,用于优化轻质复合材料可折叠管状杆的扣扣性能
Flavia Palmeri1, Susanna Laurenzi1
1Department of Astronautical Electrical and Energy Engineering, Sapienza University of Rome, Via Salaria 851-881, 00138 Rome, Italy.
Biomimetics (Basel, Switzerland)
|August 28, 2024
概括
我们开发了神经网络替代模型,以预测可折叠管状杆 (CTM) 中的曲负载. 这大大加快了优化,超薄的CTM的设计过程,增强了结构完整性.
科学领域:
- 航空航天工程 航空航天工程
- 结构力学 结构力学
- 计算科学 计算科学
背景情况:
- 可折叠管状杆 (CTM) 是太空应用中的关键结构元素.
- 超薄的CTM在轴和曲负荷下容易受到局部曲的影响,这挑战了传统的设计.
- 预测曲行为是复杂的,因为截面几何和故障模式之间的复杂关系.
研究的目的:
- 开发准确且计算效率高的替代模型,用于预测CTM的非线性曲折行为.
- 实现CTM截面的多目标优化 (MOO),以提高稳定性和承载能力.
- 通过减少分析时间,加快超薄CTM的设计周期.
主要方法:
- 使用有限元分析 (FEA) 来生成CTM的曲折负载数据.
- 开发基于神经网络 (NN) 的替代模型,在FEA数据上进行训练.
- 集成的NN代孕模型与MOO的非主导排序遗传算法II (NSGA-II).
主要成果:
- 在NN的替代模型中,对曲负荷 (R2值高达0.9987) 实现了高预测准确度.
- 预测时间从几分钟 (FEA) 减少到几分之一秒,大大提高了计算效率.
- 确定了1000个非主导的CTM截面配置,通过MOO优化曲性能.
结论:
- 基于NN的替代模型提供了一个非常准确和高效的方法来预测CTM曲行为.
- 提出的方法有助于设计结构优化和稳定的超薄CTM.
- 这种方法可以为先进的航空航天结构做出明智的设计决策.
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