[2] 郝英,孙建国,杨国庆,等.基于支持向量机的民航发动机故障检测研究[J].航空学报,2005,26(4):434-438. [3] Volponi A, DePold H, Ganguli R, et al, The use of Kalman filter and neural network methodologies in gas turbine performance diagnostics:a comparative study[J].ASME Journal of Engineering for Gas Turbine and Power,2003,125(4):917-924. [4] Batcho P F, Moller J C, Padova C, et al.Interpretation of gas turbine response due to dust ingestion[J].Journal of Engineering for Gas Turbines and Power,7,9(3):344-352. [5] Kobayashi T,Simon D L.Evaluation of an enhanced bank of Kalman filters for in-flight aircraft engine sensor fault diagnostics[R].NASA/TM_2004-213203. [6] Lakshminarasimha A N, Boyce M P, Meher-Homji C B.Modeling and analysis of gas turbine performance deterioration[J].Journal of Engineering for Gas Turbines and Power,4,6(1):46-52. [7] Diakunchak I S.Performance detrioration in industrial gas turbines[J].Journal of Engineering for Gas Turbines and Power,2,4(2):161-168. [8] Tabakoff W, Lakshminarasimha A N,Pasin M.Simulation of compressor performance deterioration due to erosion[J].Journal of Turbomachinery,0,2(1):78-83. [9] Richardson J H, Sallee G P, Smakula F K.Causes of high pressure compressor detrioration in service[R].AIAA 79-1234. [10] Lambert H H.A simulation study of turbofan engine deterioration estimation using Kalman filter techniques[R].NASA-TM-104233. [11] Xue Wei, Guo Yingqing.Aircraft engine sensor fault diagnostics based on estimation of engines health degradation[J].Chinese Journal of Aeronautics,9,2(1):18-21. [12] 薛薇,郭迎清.采用序列概率比方法检测航空发动机传感器软故障[J].航空动力学报,2007,22(11):1925-1929. [13] Xue Wei, Guo Yingqing, Zhang Xiaodong.Application of a bank of Kalman filters and a robust Kalman filter for aircraft engine sensor/actuator fault diagnosis[J].International Journal of Innovative Computing Information and Control,8,4(12):3161-3168.
|