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航空发动机三变量鲁棒控制器设计
引用本文:王前宇,孙健国,李秋红.航空发动机三变量鲁棒控制器设计[J].航空动力学报,2009,24(11):2607-2611.
作者姓名:王前宇  孙健国  李秋红
作者单位:南京航空航天大学,能源与动力学院,南京,210016
摘    要:对发动机三变量控制进行了研究.由于发动机可作为被控量的输出参数很多,用不同的被控量设计的控制器系统性能差别很大,所以选择合适的被控量就显得尤为重要.采用RSCN(鲁棒稳定性和条件数)方法从发动机的14个输出变量中选择三个变量作为发动机的被控量,然后用所选择的发动机输入/输出变量来设计增广LQR(1inenr quadratic requlator)控制器,数字仿真表明通过上述方法设计的发动机控制系统响应速度较快,无稳态误差,鲁棒性好.

关 键 词:航空发动机  输入输出选择  控制结构设计  增广LQR控制器
收稿时间:2008/11/5 0:00:00
修稿时间:2009/1/11 0:00:00

Three-variables robust controller design for aero-engine
WANG Qian-yu,SUN Jian-guo and LI Qiu-hong.Three-variables robust controller design for aero-engine[J].Journal of Aerospace Power,2009,24(11):2607-2611.
Authors:WANG Qian-yu  SUN Jian-guo and LI Qiu-hong
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:Three variables controller for aero-engine was studied in this paper.Given the fact that too many outputs of aero-engine could be used as controlled variables,and different controlled variables have varying performances,it is particularly important to get the suitable controlled variables.Here,the method of choosing best outputs as the controlled variables is RSCN(robust stability and condition number)method.Three output-variables were chosen from 14 outputs of aero-engine.After the selection of controlled variables was completed,an augmented LQR(linenr quadratic requlator) controller was designed.The simulation indicates that the controller with the chosen outputs gets very well dynamic and steady state performance.
Keywords:aero-engine  input-output select  control structure design  augmented LQR(linear quadratic requlator) controller
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