基于增益调度的航空发动机分散鲁棒控制

doi:10.13700/j.bh.1001-5965.2017.0659

北京航空航天大学学报 ›› 2018, Vol. 44 ›› Issue (9): 1964-1973.doi: 10.13700/j.bh.1001-5965.2017.0659

基于增益调度的航空发动机分散鲁棒控制

潘慕绚, 曹良进, 黄金泉

南京航空航天大学能源与动力学院江苏省航空动力系统重点实验室, 南京 210016

收稿日期:2017-10-24 出版日期:2018-09-20 发布日期:2018-09-21
通讯作者: 潘慕绚.E-mail:muxuan.pan@nuaa.edu.cn E-mail:muxuan.pan@nuaa.edu.cn
作者简介:潘慕绚女,博士,副教授,硕士生导师。主要研究方向:航空发动机控制系统设计及仿真;曹良进男,硕士研究生。主要研究方向:航空发动机控制系统设计及仿真。
基金资助:
国家自然科学基金（51406084）；江苏省航空动力系统重点实验室基金（NJ20160020）

Gain scheduling based decentralized robust control for aircraft engines

PAN Muxuan, CAO Liangjin, HUANG Jinquan

Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received:2017-10-24 Online:2018-09-20 Published:2018-09-21
Supported by:
National Natural Science Foundation of China (51406084); Foudation of Jiangsu Province Key Laboratory of Aerospace Power System (NJ20160020)

摘要/Abstract

摘要： 针对航空发动机全包线大范围非线性变化动态特性下的跟踪控制问题，设计分散鲁棒跟踪控制器。引入动态响应指数收敛参数，使得控制器在保证系统稳定的同时跟踪误差收敛速率可调。在飞行包线内选择一系列设计点，以油门杆角度（PLA）表征发动机功率水平，每隔5°选取一个PLA 作为一个设计功率水平，针对从一个设计功率水平过渡到另一个设计功率水平的设计阶跃过程，采用递进法设计分散鲁棒跟踪控制器。采用线性插值的方法调度非设计阶跃过程分散鲁棒跟踪控制器参数。针对某型涡扇发动机部件级模型进行仿真，仿真结果验证了控制方法的有效性。

关键词: 航空发动机, 全包线, 跟踪控制, 分散鲁棒控制, 增益调度

Abstract: Considering the aircraft engine full envelope tracking control under the nonlinear variation dynamic feature within wide range, the decentralized robust tracking controller is proposed. In order to ensure system stability and at the same time make the convergent rates of tracking errors adjustable, the dynamic response exponential convergent parameter is introduced. A set of operating points in the full envelope are chosen, and the aircraft engine power level is denoted by power lever angle (PLA). For every 5°, a PLA is chosen as a design power level. A design step process is described by a process in which the aircraft engine transfers from initial design power level to another design power level. Considering every design step process, a decentralized robust tracking controller was designed based on "stepping method". The parameters of decentralized robust tracking controller in off-design step process were scheduled by linear interpolation. A simulation was conducted on component-level model of a certain type of turbofan engine. The results validate the effectiveness of the control method.

Key words: aircraft engine, full envelope, tracking control, decentralized robust control, gain scheduling

中图分类号:

V233.7

潘慕绚, 曹良进, 黄金泉. 基于增益调度的航空发动机分散鲁棒控制[J]. 北京航空航天大学学报, 2018, 44(9): 1964-1973.

PAN Muxuan, CAO Liangjin, HUANG Jinquan. Gain scheduling based decentralized robust control for aircraft engines[J]. JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2018, 44(9): 1964-1973.

参考文献

[1] JAMSHID M.Large-scale systems:Modeling and control[M].New York:Elsevier,1983:188.
[2] SABATTO S Z,MGAYA R,BODRUZZAMANM.Modeling and simulation studies of a decentralized architecture for a distributed turbine engine controls[C]//47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Reston:AIAA,2011:6011.
[3] PEREZ R A,LOU K N.Decentralised multivariable control and stability of a gas turbine engine[J].IEEE Proceedings-Control Theory and Applications,1994,141(6):357-366.
[4] ZECEVIC A I,NESKOVIC G,SILJAK D D.Robust decentralized exciter control with linear feedback[J].IEEE Transactions on Power Systems,2004,19(2):1096-1103.
[5] CHENG C W,WU Q,ALEXANDER T T.Decentralized robust controller design for uncertain large-scale systems with control delays[J].International Journal of Systems Science,2001,32(1):33-41.
[6] PANDIAN S R,HANMANDLU M.Decentralized model-based control of a class of large-scale interconnected systems[J].International Journal of Systems Science,1993,24(3):499-514.
[7] WU H S.Decentralised adaptive controllers for robust tracking and model following of uncertain large scale systems[J].International Journal of Control,2009,82(2):268-278.
[8] WU H S.Decentralised adaptive robust control of uncertain large-scale non-linear dynamical systems with multiple time-varying delays[J].IET Control Theory & Applications,2012,6(5):629-640.
[9] CHEN Y H.Decentralized robust output and estimated state feedback controls for large-scale uncertain systems[J].International Journal of Control,1987,46(6):1979-1992.
[10] HA Q P,TRINH H.Observer-based control of multi-agent systems under decentralized information structure[J].International Journal of Systems Science,2004,35(12):719-728.
[11] ELMAHDI A,TAHA A F,SUN D F.Observer-based decentralized control scheme for stability analysis of networked systems[C]//11th IEEE International Conference on Control & Automation.Piscataway,NJ:IEEE Press,2015:862-875.
[12] TSENG C S,CHEN B S.H_∞ decentralized fuzzy model reference tracking control design for nonlinear interconnected systems[J].IEEE Transactions on Fuzzy Systems,2001,9(6):795-809.
[13] TONG S C,LIU C L,LI Y M.Fuzzy-adaptive decentralized output-feedback control for large-scale nonlinear systems with dynamical uncertainties[J].IEEE Transactions on Fuzzy Systems,2010,18(5):845-861.
[14] TONG S C,LI Y M,ZHANG H G.Adaptive neural network decentralized backstepping output-feedback control for nonlinear large-scale systems with time delays[J].IEEE Transactions on Neural Networks,2011,22(7):1073-1086.
[15] CHEN Y H.Decentralized robust control system design for large-scale uncertain systems[J].International Journal of Control,1988,47(5):1195-1205.
[16] HAN M C,CHEN Y H.Decentralized control design:Uncertain systems with strong interconnections[J].International Journal of Control,1995,61(6):1363-1385.
[17] UDWADIA F E,KOGANTIP B,WANICHANON T,et al.Decentralised control of nonlinear dynamical systems[J].International Journal of Control,2014,87(4):827-843.
[18] LIN S T,LEE C M.Multivariable control of the J-85 turbojet engine for full flight envelope operation[J].Journal of Guidance,Control,and Dynamics,2012,19(4):913-920.
[19] 李嘉,李华聪,徐轩,等.航空发动机多变量变增益控制器设计及仿真[J].北京航空航天大学学报,2016,42(9):1958-1968.LI J,LI H C,XU X,et al.Multi-variable variable gain controller design and simulation based on aero engine[J].Journal of Beijing University of Aeronautics and Astronautics,2016,42(9):1958-1968(in Chinese).
[20] 隋岩峰,于达仁,隋鹏.涡扇发动机自增益调度H_∞控制器设计[J].航空动力学报,2005,20(5):857-861.SUI Y F,YU D R,SUI P.Design of self-scheduled H_∞ control for turbofan engine[J].Journal of Aerospace Power,2005,20(5):857-861(in Chinese).
[21] 姚华,鲍亮亮,孙健国.基于神经网络的航空发动机全包线PID控制[J].南京航空航天大学学报,2007,39(2):236-239.YAO H,BAO L L,SUN J G.Aeroengine PID control over whole envelope based on neural network[J].Journal of Nanjing University of Aeronautics and Astronautics,2007,39(2):236-239(in Chinese).
[22] 王海泉,郭迎清,李睿,等.航空发动机全飞行包线鲁棒控制器设计研究[J].测控技术,2009,28(5):48-51.WANG H Q,GUO Y Q,LI R,et al.Design of full flight envelope controller for aero-engine[J].Journal of Measurement and Control Technology,2009,28(5):48-51(in Chinese).
[23] 吴斌,黄金泉.航空发动机全包线鲁棒变增益LPV控制律设计[J].南京航空航天大学学报,2014,46(2):252-258.WU B,HUANG J Q.Robust gain scheduling LPV control design for aeroengine in full envelope[J].Journal of Nanjing University of Aeronautics and Astronautics,2014,46(2):252-258(in Chinese).
[24] 吴斌,黄金泉.航空发动机增益调度控制的多项式平方和规划方法[J].航空动力学报,2016,31(6):1460-1468.WU B,HUANG J Q.Self-Scheduled control method for aero-engine based on sum of squares programming of polynomial[J].Journal of Aerospace Power,2016,31(6):1460-1468(in Chinese).
[25] 吴斌,黄金泉.基于切换多胞LPV的涡扇发动机全包线中间状态控制[J].航空动力学报,2016,31(8):2040-2048.WU B,HUANG J Q.Intermediate state control of turbofan engine in full envelope based on switched polytopic LPV approach[J].Journal of Aerospace Power,2016,31(8):2040-2048(in Chinese).
[26] BOYD S,GHAOUI L E,FERON E,et al.Linear matrix inequality in system and control theory[M]//SIAM Studies in Applied Mathematics.Philadelphia:SIAM,1994:28.
[27] PETERSEN I R,HOLLOTH C V.A Riccati equation approach to the stabilization of uncertain linear systems[J].Automatica,1986,22(4):397-411.

基于增益调度的航空发动机分散鲁棒控制

Gain scheduling based decentralized robust control for aircraft engines

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