A switching control strategy of safety protection problem for aero-engines
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- 英文论文题名：A switching control strategy of safety protection problem for aero-engines
- 论文作者：Shi Yan ; Zhao Jun
- 英文论文作者：Shi Yan ; Zhao Jun ; State Key Laboratory of Synthetical Automation for Process Industries (Northeastern University) ; College of Information Science and Engineering ; Northeastern University
- 年：2017
- 作者机构：State Key Laboratory of Synthetical Automation for Process Industries (Northeastern University),College of Information Science and Engineering,Northeastern University;
- 英文论文关键词：Aero-engine ; switching control ; equilibrium manifold expansion(EME) ; safety protection ; sliding mode control(SMC)
- 会议召开时间：2017-07-26
- 会议录名称：第36届中国控制会议论文集（A）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（A）
- 语种：英文
- 分类号：V233.7
- 学会代码：KZLL
- 会议名称：第36届中国控制会议
- 会议地点：中国辽宁大连
- 主办单位：中国自动化学会控制理论专业委员会
- 学会名称：中国自动化学会控制理论专业委员会
- 页数：5
- 文件大小：260k
- 原文格式：D
- 会议级别：全国
摘要
This paper focuses on a switching control of the temperature protection problem for aero-engines. Firstly, an equilibrium manifold expansion(EME) model is established to describe the aero-engine for high accuracy. Then, a speed regulation controller is designed to obtain the asymptotic stability. As the temperature measurements usually have errors for aero-engines, a safety protection control strategy based on the sliding mode control(SMC) is proposed. It can avoid the over-temperature problem for aero-engines, furthermore, possess the disturbance-resistant performance. Then we design an appropriate switching law which makes the aero-engine have a fast transient response speed without exceeding the safety boundary. Finally, a simulation of a two-spool turbofan engine model is given to demonstrate the effectiveness of the proposed method.
This paper focuses on a switching control of the temperature protection problem for aero-engines. Firstly, an equilibrium manifold expansion(EME) model is established to describe the aero-engine for high accuracy. Then, a speed regulation controller is designed to obtain the asymptotic stability. As the temperature measurements usually have errors for aero-engines, a safety protection control strategy based on the sliding mode control(SMC) is proposed. It can avoid the over-temperature problem for aero-engines, furthermore, possess the disturbance-resistant performance. Then we design an appropriate switching law which makes the aero-engine have a fast transient response speed without exceeding the safety boundary. Finally, a simulation of a two-spool turbofan engine model is given to demonstrate the effectiveness of the proposed method.
This paper focuses on a switching control of the temperature protection problem for aero-engines. Firstly, an equilibrium manifold expansion(EME) model is established to describe the aero-engine for high accuracy. Then, a speed regulation controller is designed to obtain the asymptotic stability. As the temperature measurements usually have errors for aero-engines, a safety protection control strategy based on the sliding mode control(SMC) is proposed. It can avoid the over-temperature problem for aero-engines, furthermore, possess the disturbance-resistant performance. Then we design an appropriate switching law which makes the aero-engine have a fast transient response speed without exceeding the safety boundary. Finally, a simulation of a two-spool turbofan engine model is given to demonstrate the effectiveness of the proposed method.
引文
[1]L.C.Jaw,Aircraft engine controls design,system analysis,and health monitoring.In AIAA Education Series,2009.
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[5]N.V.Kulkarni,K.Krishna Kumar,Intelligent engine control using an adaptive critic.IEEE Transactions on Control Systems Technology,11(2),164C173,2003.
[6]H.Richter,Advanced control of turbofan engines.Springer,New York,2012.
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[10]X.M.Sun,J.Zhao,D.J.Hill,Stability and L-2-gain analysis for switched delay systems:A delay-dependent method,Automatica,10(42):1769C1774,2006.
[11]J.Zhao,D.J.Hill,On stability,L2-gain and H∞control for switched systems,Automatica,5(44):1220-1232,2008.
[12]Y.Qi,W.Bao,Q.Zhang,R.Cao,Command switching based multiobjective safety protection control for inlet buzz of scramjet engine,Journal of the Franklin Institute,11(352):5191–5213,2015.
[13]C.Chen,Y.Sui,J.Zhao,Coordinated switching control of thrust tracking and safety protection for aero-engines.Proceedings of 33rd Chinese Control Conference,2014:4050–4055.
[14]X.Liu,J.Shi,Y.Qi,Y.Yuan,Design for aircraft engine multi-objective controllers with switching characteristics.Chinese Journal of Aeronautics,27(5):1097-1110,2014.
[15]H.Richter,A multi-regulator sliding mode control strategy for output-constrained systems.Automatica,47(10):2251-2259,2011.
[16]X.Liu,L.Zhao,Modeling of gas turbine engine compressor surge based on equilibrium manifold,Proceedings of International Conference on Control Engineering and Communication Technology,2012:300–306.
[17]Y.Shi,J.Zhao,Y.Liu,Switching control for aero-Engines based on switched equilibrium manifold expansion model.IEEE Transactions on Industrial Electronics,4(64):3156–3165,2017.
[18]D.J.Stilwell,W.J.Rugh,Interpolation of observer state feedback controllers for gain scheduling,IEEE Transactions on Automatic Control,6(44):1225–1229,1999.
[2]H.A.Spang III,H.Brown,Control of jet engines.Control Engineering Practice,7(9):1043-1059,1999.
[3]J.Meyer,S.Yurkovich,S.Midlam-Mohler,Air-to-fuel ratio switching frequency control for gasoline engines.IEEE Transactions on Control Systems Technology,3(21):636-648,2013.
[4]A.J.Chipperfield,B.Bica,P.J.Fleming,Fuzzy scheduling control of a gas turbine aero-engine:A multiobjective approach.IEEE Transactions on Industrial Electronics,49(3):536C548,2002.
[5]N.V.Kulkarni,K.Krishna Kumar,Intelligent engine control using an adaptive critic.IEEE Transactions on Control Systems Technology,11(2),164C173,2003.
[6]H.Richter,Advanced control of turbofan engines.Springer,New York,2012.
[7]L.C.Jaw,J.D.Mattingly,Aircraft Engine Controls.American Institute of Aeronautics and Astronautics Reston,VA,2009.
[8]K.S.Narendra,J.Balakrishnan,A Common Lyapunov Function for Stable LTI Systems with Commuting A-Matrices,IEEE Transactions on Automatic Control,12(39):2469–2471,1994.
[9]K.Tanaka,T.Hori,H.O.Wang,A multiple Lyapunov function approach to stabilization of fuzzy control systems,IEEE Transactions on Fuzzy Systems,4(11):582–589,2003.
[10]X.M.Sun,J.Zhao,D.J.Hill,Stability and L-2-gain analysis for switched delay systems:A delay-dependent method,Automatica,10(42):1769C1774,2006.
[11]J.Zhao,D.J.Hill,On stability,L2-gain and H∞control for switched systems,Automatica,5(44):1220-1232,2008.
[12]Y.Qi,W.Bao,Q.Zhang,R.Cao,Command switching based multiobjective safety protection control for inlet buzz of scramjet engine,Journal of the Franklin Institute,11(352):5191–5213,2015.
[13]C.Chen,Y.Sui,J.Zhao,Coordinated switching control of thrust tracking and safety protection for aero-engines.Proceedings of 33rd Chinese Control Conference,2014:4050–4055.
[14]X.Liu,J.Shi,Y.Qi,Y.Yuan,Design for aircraft engine multi-objective controllers with switching characteristics.Chinese Journal of Aeronautics,27(5):1097-1110,2014.
[15]H.Richter,A multi-regulator sliding mode control strategy for output-constrained systems.Automatica,47(10):2251-2259,2011.
[16]X.Liu,L.Zhao,Modeling of gas turbine engine compressor surge based on equilibrium manifold,Proceedings of International Conference on Control Engineering and Communication Technology,2012:300–306.
[17]Y.Shi,J.Zhao,Y.Liu,Switching control for aero-Engines based on switched equilibrium manifold expansion model.IEEE Transactions on Industrial Electronics,4(64):3156–3165,2017.
[18]D.J.Stilwell,W.J.Rugh,Interpolation of observer state feedback controllers for gain scheduling,IEEE Transactions on Automatic Control,6(44):1225–1229,1999.