[1] 费成巍,艾延廷.航空发动机健康管理系统设计技术[J].航空发动机, 2009,5(5):24-29.
[2] 《航空发动机设计手册》总编委会.航空发动机设计手册(第19册):转子动力学及整机振动[M].北京:航空工业出版社, 2001.
[3] Lin Jing, Qu Liang-sheng.Feature Extraction Based on Morlet Wavelet and Its Application for Mechanical Fault Diagnosis [J].Journal of Sound and Vibration, 2000,4(1):135-148.
[4] Chebil J, Noel G, Mesbah M, et al.Wavelet Decomposition for the Detection and Diagnosis of Faults in Rolling Element Bearings [J].Jordan Journal of Mechanical and Industrial Engineering, 2009,3(4):260-267.
[5] 艾延廷, 费成巍.转子振动故障的小波能谱熵SVM故障诊断[J].航空动力学报,2011,6(8):1830-1835.
[6] 曾庆虎, 刘冠军, 邱静.基于小波相关特征尺度熵的预测特征信息提取方法研究[J].中国机械工程, 2008,9(10):1193-1196.
[7] 赵冲冲, 廖明夫, 于萧.基于支持向量机的旋转机械故障诊断[J].振动、测试与诊断, 2006,6(1).
[8] 费成巍, 白广忱, 李晓颖.基于过程功率谱熵SVM的转子振动故障诊断方法[J].推进技术, 2012,3(2):293-298.(FEI Cheng-wei, BAI Guang-chen, LI Xiao-ying.Method of Rotor Vibration Fault Diagnosis From Process Power Spectrum Entropy and SVM[J].Journal of Propulsion Technology, 2012,3(2).
[9] 艾延廷, 费成巍.基于支持向量机的转子振动故障融合诊断技术[J].沈阳工业大学学报, 2010,2(5).
[10] LI Jun-tao, JIA Ying-min.Huberized Multiclass Support Vector Machine for Microarray Classification [J].Acta Automatica Sinica, 2010,6(3):399-405.
[11] LIN Chun-fu, WANG Sheng-de.Fuzzy Support Vector Machines [J].IEEE Transactions On Neural Networks, 2002,3(2):464-471.
[12] Tsujinishi D, Abe S.Fuzzy Least Squares Support Vector Machines for Multiclass Problem [J].Neural Networks, 2003:16(5-6):785-792.
[13] LIN Chun-fu, WANG Sheng-de.Training Algorithms for Fuzzy Support Vector Machines with Noisy Data [J].Pattern Recognition Letters, 2004,5(14):1647-1656.
[14] MAO Yong, XIA Zheng, YIN Zheng, et al.Fault Diagnosis Based on Fuzzy Support Vector Machine with Parameter Tuning and Feature Selection[J].Chinese Journal of Chemical Engineering, 2007,5(2):233-239.
[15] 艾延廷, 费成巍.基于改进模糊SVM的转子振动故障诊断 [J].航空动力学报, 2011,6(5):1118-1123.
[16] 郭秩维, 费成巍, 白广忱.基于FSVM改进隶属度的发动机振动性能分析[J].推进技术, 2013,4(2):263-267.( GUO Zhi-wei, FEI Cheng-wei, BAI Guang-chen.Improved Fuzzy Membership in FSVM for Aeroengine Vibration Performance Fusion Analysis[J].Journal of Propulsion Technology, 2013,4(2):263-268.
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