Design of non-fully recover LQG/LTR control system of aeroengine

WANG Yong-ting; GUO Ying-qing; WANG Hai-quan

Chinese

您当前的位置：

首页 >

文章列表页 >

Design of non-fully recover LQG/LTR control system of aeroengine

更新时间：2026-07-07

- Design of non-fully recover LQG/LTR control system of aeroengine
- Vol. 22, Issue 3, (2007)
- 作者机构：
  
  西北工业大学动力与能源学院,西安,710072
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2007
- 稿件说明：
移动端阅览
WANG Yong-ting, GUO Ying-qing, WANG Hai-quan. Design of non-fully recover LQG/LTR control system of aeroengine[J]. 2007, 22(3).
DOI：

WANG Yong-ting, GUO Ying-qing, WANG Hai-quan. Design of non-fully recover LQG/LTR control system of aeroengine[J]. 2007, 22(3). DOI：

摘要

为解决常规LQG/LTR控制器中存在的参数值过大问题

提出了非完全恢复的LQG/LTR设计方法

并从控制系统中零极点关系的角度

阐述了该设计方法降低控制器参数数值的机理.将该方法应用于航空发动机控制系统设计中.仿真表明

该方法不但有效地抑制了控制器的参数值过大

且相对于常规LQG/LTR设计方法具有更理想的控制效果.

Abstract

To solve the problem of excessively big parameter value in the conventional LQG/LTR controller

a design method was proposed for non-fully recover LQG/LTR.The principle for reducing the controller parameter value was explained from the perspective of system's zero-pole relationship.This method was applied to design the aeroengine control system.Simulation results indicate that this method could suppress effectively the parameter value of controller

but also present more satisfactory performance than conventional LQG/LTR design method.

关键词

Keywords

references

Views

434

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Automatic code generation technology for control method based on RTWEC

Augmented LQL method and its application to aeroengine control

Stability analysis and improvement of ZP/LTR method of aeroengine

Theory of Similarity Based Aeroengine Multivariable Control Method

Augmented LQR Method for Aeroengine Control Systems

Related Author

LU Jun

WANG Bin-zheng

WANG Hai-guan

YANG Gang

YAO Hua

YANG Gang

YAO Hua

YANG Gang

Related Institution

Aviation Motor Control System Institute

Aviation Motor Control System Institute, China Aviation Industry Corporation Ⅰ

Nanjing University of Aeronautics and Astronautics

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

Department of Power and Propulsion, School of Engineering, Cranfield University, Bedfordshire MK4

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰