A Strong Tracking Filtering Approach for Health Estimation of Marine Gas Turbine Engine

Qingcai Yang , Shuying Li , Yunpeng Cao

Journal of Marine Science and Application ›› 2019, Vol. 18 ›› Issue (4) : 542 -553.

PDF
Journal of Marine Science and Application ›› 2019, Vol. 18 ›› Issue (4) : 542 -553. DOI: 10.1007/s11804-019-00103-8
Research Article

A Strong Tracking Filtering Approach for Health Estimation of Marine Gas Turbine Engine

Author information +
History +
PDF

Abstract

Monitoring and evaluating the health parameters of marine gas turbine engine help in developing predictive control techniques and maintenance schedules. Because the health parameters are unmeasurable, researchers estimate them only based on the available measurement parameters. Kalman filter-based approaches are the most commonly used estimation approaches; however, the conventional Kalman filter-based approaches have a poor robustness to the model uncertainty, and their ability to track the mutation condition is influenced by historical data. Therefore, in this paper, an improved Kalman filter-based algorithm called the strong tracking extended Kalman filter (STEKF) approach is proposed to estimate the gas turbine health parameters. The analytical expressions of Jacobian matrixes are deduced by non-equilibrium point analytical linearization to address the problem of the conventional approaches. The proposed approach was used to estimate the health parameters of a two-shaft marine gas turbine engine in the simulation environment and was compared with the extended Kalman filter (EKF) and the unscented Kalman filter (UKF). The results show that the STEKF approach not only has a computation cost similar to that of the EKF approach but also outperforms the EKF approach when the health parameters change abruptly and the noise mean value is not zero.

Keywords

Gas turbine / Health parameter estimation / Extended Kalman filter / Unscented Kalman filter / Strong tracking Kalman filter / Analytical linearization

Cite this article

Download citation ▾
Qingcai Yang, Shuying Li, Yunpeng Cao. A Strong Tracking Filtering Approach for Health Estimation of Marine Gas Turbine Engine. Journal of Marine Science and Application, 2019, 18(4): 542-553 DOI:10.1007/s11804-019-00103-8

登录浏览全文

4963

注册一个新账户 忘记密码

References

[1]

Borguet S, Léonard O. Comparison of adaptive filters for gas turbine performance monitoring. Journal of Computational & Applied Mathematics, 2010, 234(7): 2202-2212

[2]

Brotherton T, Volponi A, Luppold R, Simon DL (2003) eSTORM: enhanced self-tuning on-board real-time engine model. In: Proceedings of the 2003 IEEE aerospace conference, Big Sky, 3075–3086. https://doi.org/10.1109/AERO.2003.1234150

[3]

Camporeale SM, Fortunato B, Mastrovito M. A modular code for real time dynamic simulation of gas turbines in Simulink. J Eng Gas Turbines Power, 2006, 128(3): 506-517

[4]

Chang Xiaodong, Huang Jinquan, Lu Feng, Sun Haobo. Gas-Path Health Estimation for an Aircraft Engine Based on a Sliding Mode Observer. Energies, 2016, 9(8): 598

[5]

Johansen TA, Hunt KJ, Gawthrop PJ, Fritz H. Off-equilibrium linearisation and design of gain-scheduled control with application to vehicle speed control. Control Eng Pract, 1998, 6(2): 167-180

[6]

Kerr LJ, Nemec TS, Gallops GW. Real-time estimation of gas turbine engine damage using a control-based Kalman filter algorithm. J Eng Gas Turbines Power, 1992, 114(2): 187-195

[7]

Klapproth J, Miller M, Parker D (1979) Aerodynamic development and performance of CF6-6/LM2500 compressor. In: Proceedings of 4th international symposium on air breathing engines, Orlando, 243–249. https://doi.org/10.2514/6.1979-7030

[8]

Kobayashi T, Simon DL, Litt JS (2005) Application of a constant gain extended Kalman filter for in-flight estimation of aircraft engine performance parameters. In: Proceedings of ASME Turbo expo 2005: power for land, sea, and air, Reno, 617–628. https://doi.org/10.1115/GT2005-68494

[9]

Lambert HH (1991) A simulation study of turbofan engine deterioration estimation using Kalman filtering techniques. NASA Technical Memorandum 104233

[10]

Li YG. Gas turbine performance and health status estimation using adaptive gas path analysis. J Eng Gas Turbines Power, 2010, 132(4): 109-121

[11]

Li YG, Korakiantis T. Nonlinear weighted least squares estimation approach for gas-turbine diagnostic applications. Journal of Propulsion & Power, 2012, 27(2): 337-345

[12]

Li YG, Pilidis P. Ga-based design-point performance adaptation and its comparison with icm-based approach. Appl Energy, 2010, 87(1): 340-348

[13]

Lu F, Huang J, Lv Y. Gas path health monitoring for a turbofan engine based on a nonlinear filtering approach. Energies, 2013, 6(1): 492-513

[14]

Luppold RH, Roman JR, Gallops GW (1989) Estimating in-flight engine performance variations using Kalman filter concepts. Proceeding of the 25th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Monterey, 1–10. https://doi.org/10.2514/6.1989-2584

[15]

Pu X, Liu S, Jiang H, Yu D. Adaptive gas path diagnostics using strong tracking filter. Proc IMechE, Part G: Journal of Aerospace Engineering, 2013, 228(4): 577-585

[16]

Rahme S, Meskin N. Adaptive sliding mode observer for sensor fault diagnosis of an industrial gas turbine. Control Eng Pract, 2015, 38: 57-74

[17]

Simon D (2006) H filtering with inequality constraints for aircraft turbofan engine health estimation. In: Proceedings of the 45th IEEE conference on decision and control, San Diego, CA, 3291–3296. https://doi.org/10.1109/CDC.2006.376880

[18]

Simon D. A comparison of filtering approaches for aircraft engine health estimation. Aerosp Sci Technol, 2008, 12(2): 276-284

[19]

Simon DL, Garg S. Optimal tuner selection for Kalman filter-based aircraft engine performance estimation. J Eng Gas Turbines Power, 2010, 132(3): 659-671

[20]

Simon D, Simon DL. Aircraft turbofan engine health estimation using constrained Kalman filtering. J Eng Gas Turbines Power, 2005, 127(2): 323-328

[21]

Simon D, Simon DL. Kalman filter constraint switching for turbofan engine health estimation. Eur J Control, 2006, 12(3): 331-343

[22]

Simon D, Simon DL. Constrained Kalman filtering via density function truncation for turbofan engine health estimation. Int J Syst Sci, 2010, 41(2): 159-171

[23]

Tsoutsanis E, Meskin N, Benammar M, Khorasani K (2013) Dynamic performance simulation of an aeroderivative gas turbine using the Matlab Simulink environment. In: Proceedings of ASME 2013 international mechanical engineering congress and exposition, San Diego, CA, 1–10. https://doi.org/10.1115/IMECE2013-64102

[24]

Volponi AJ. Gas turbine engine health management: past, present and future trends. J Eng Gas Turbines Power, 2013, 58(136): 433-455

[25]

Volponi A, DePold H, Ganguli R, Daguang C. The use of Kalman filter and neural network methodologies in gas turbine performance diagnostics: a comparative study. J Eng Gas Turbines Power, 2003, 125(4): 917-924

[26]

Yang X, Shen W, Pang S, Li B, Jiang K, Wang Y. A novel gas turbine engine health status estimation approach using quantum behaved particle swarm optimization. Math Probl Eng, 2014, 2014(3): 1-11

[27]

Yang Qingcai, Li Shuying, Cao Yunpeng. A new component map generation method for gas turbine adaptation performance simulation. Journal of Mechanical Science and Technology, 2017, 31(4): 1947-1957

[28]

Zhou DH, Frank PM. Strong tracking Kalman filtering of nonlinear time-varying stochastic systems with coloured noise: application to parameter estimation and empirical robustness analysis. Int J Control, 1996, 65(2): 295-307

AI Summary AI Mindmap
PDF

162

Accesses

0

Citation

Detail

Sections
Recommended

AI思维导图

/