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基于支持向量机的航空发动机PID解耦控制
引用本文:吴勇,谢寿生,唐奇,武卫,王海涛,苗卓广. 基于支持向量机的航空发动机PID解耦控制[J]. 航空动力学报, 2009, 24(10): 2349-2355
作者姓名:吴勇  谢寿生  唐奇  武卫  王海涛  苗卓广
作者单位:1.空军工程大学工程学院, 西安 710038
摘    要:针对航空发动机多变量控制系统中各回路之间存在的耦合现象,提出了一种基于支持向量机(support vector machines,SVM)的航空发动机PID(proportion integration differentiation)解耦控制方法.利用SVM辨识发动机非线性模型,并获得SVM瞬时线性化模型,在线性化模型的基础上完成了PID参数的在线自整定.利用Lyapunov稳定性定理对控制器的收敛性进行了分析.通过对某型航空发动机的仿真,验证了该方法的有效性和可行性. 

关 键 词:支持向量机  线性化  PID控制器  解耦控制  收敛性
收稿时间:2009-05-12
修稿时间:2009-07-22

PID decoupling controller for aero-engine based on support vector machines
WU Yong,Xie Shou-sheng,TANG Qi,WU Wei,WANG Hai-tao and MIAO Zhuo-guang. PID decoupling controller for aero-engine based on support vector machines[J]. Journal of Aerospace Power, 2009, 24(10): 2349-2355
Authors:WU Yong  Xie Shou-sheng  TANG Qi  WU Wei  WANG Hai-tao  MIAO Zhuo-guang
Affiliation:1.The Engineering Institute, Air Force Engineering University, Xi'an 710038, China2.Aireforce Deputation Agency in Beijing District, Beijing 100074, China
Abstract:To solve the coupling problem in aero-engine multivariable control system,a new PID(proportion integration differentiation) decoupling controller based on support vector machines(SVM) was proposed.The SVM was applied to identify the aero-engine model,and then linearized to extract the instantaneous linear model.The PID parameter was obtained based on the linear model.The convergence of PID decoupling controller was proved with the help of Lyapunov stability theorem.Simulation results of certain aero-engine system demonstrate the effectiveness and feasibility of the PID decoupling controller based on SVM.
Keywords:support vector machines   linearization   PID(proportion integration differentiation) controller   decoupling control   convergence
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