基于改进MGM(1, n)的飞机健康预报方法研究

Jianguo Cui, Desheng Song, Shiliang Dong, Mingzhuo Wang, Xiaopeng Liang, Xinhe Xu
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引用次数: 1

摘要

飞机健康状态具有很强的随机性和不确定性。针对以往灰色模型不能有效预测随机信号的问题,提出了一种基于改进MGM(1, n)的飞机健康状态预测方法。采用先进的声发射(AE)技术采集健康状态信息。用小波变换对原始声发射信号进行分解。分别提取第三层小波分解低频系数的能量值、特征值和标准差构成特征向量。然后利用这些特征向量建立改进的MGM(1, n)。改进算法通过反馈预测值与实际值之间的误差来实现,从而提高了预测精度。实验表明,改进的MGM(1,n)比GM(1,1)能更准确地预测飞机尾翼疲劳裂纹,并已成功应用于飞机结构部件健康状态的预测系统中。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Research on airplane health forecast method based on the improved MGM(1, n)
There is strong randomness and uncertainty lying in the health status of airplane. Because the former grey models can not forecast the random signals efficiently, a new forecast method for the health state of airplane, based on the improved MGM(1, n), is presented in this paper. The advanced acoustic emission (AE) technique is used to collect the health state information. The original AE signals are decomposed with the wavelet transform. The energy values, eigenvalues and standard deviation of the third layer wavelet decomposition low frequency coefficients are respectively extracted to form eigenvectors. Then the improved MGM(1, n) is established by these eigenvectors. The improved algorithm is realized by feeding back the errors between the forecast values and the actual ones so as to improve the forecast precision. Experiments show that the improved MGM(1, n) can forecast the airplane stabilizer fatigue crack more accurately than the GM (1, 1). And this new method has been successfully applied to the forecast system of the health state of airplane structure components.
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