基于FCM的安全边界提取和基于ELM的航空发动机性能参数预测*

Yingshun Li, Danyang Li, Ximing Sun, X. Yi
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引用次数: 1

摘要

航空发动机性能参数安全边界是衡量航空发动机性能的重要标准之一。然而,由于个体之间的差异和工作环境之间的差异,固定的理论边界已经不能满足工程的需要。提出了一种基于模糊c均值(FCM)和极限学习机(ELM)的航空发动机性能参数安全边界提取与预测方法。首先,将预测值与实际值之间的残差作为提取安全边界的定量依据;然后利用ELM算法预测下一段时间的安全边界。该方法针对具体情况进行了改进,提高了安全边界的准确性和泛化性。仿真实例验证了该方法的有效性。
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Safety Boundary Extraction Using FCM and Prediction Using ELM for Aero-engine Performance Parameters*
The safety boundary of Aero-engine performance parameters is one of the essential criteria for measuring aero-engine performance. However, due to the differences among individuals and discrepancies among the working environments, the fixed theoretical boundary is no longer sufficient for engineering needs. In this paper, a method based on fuzzy C-means (FCM) and Extreme Learning Machine (ELM) is proposed to extract and predict the safety boundary for aero-engine performance parameters. Firstly, the residuals between the predicted values and the actual values are used as the quantitative basis to extract the safe boundary. And then the ELM algorithm is used to forecast the safety boundary for next period of time. The method mentioned in this paper enhances the accuracy and generalization of safety boundary due to improvement for specific situations. The effectiveness of this method has been verified by simulation case.
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