A Design Method for Aeroengine Robust Multivariable Digit Controller

WANG Xi; MENG Qing-ming

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A Design Method for Aeroengine Robust Multivariable Digit Controller

更新时间：2026-07-07

- A Design Method for Aeroengine Robust Multivariable Digit Controller
- Vol. 16, Issue 3, (2001)
- 作者机构：
  
  北京航空航天大学406教研室,北京,100083
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2001
- 稿件说明：
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WANG Xi, MENG Qing-ming. A Design Method for Aeroengine Robust Multivariable Digit Controller[J]. 2001, 16(3).
DOI：

WANG Xi, MENG Qing-ming. A Design Method for Aeroengine Robust Multivariable Digit Controller[J]. 2001, 16(3). DOI：

摘要

提出了一种设计发动机多变量鲁棒数字控制器的方法

即在划分的飞行包线内

控制结构采用前馈加反馈的方法

对结构不确定性和非结构不确定性进行μ结构化处理

化为H∞控制问题求解

这一方法在发动机非线形气动热力模型上进行了仿真验证。

Abstract

A method is provided for designing robust multivariable digit controller of turbojet engine

in which the forwardback and feedback control structure is adopted in the divided flight envelope

the μ structurization is used to deal with the structured uncertainty and unstructured uncertainty

so that the problem for solving robust controller is transformed into standard H∞ control problem.The robust disturbance rejection and tracking performance is verified by simulation on a nonlinear model of the twin spool turbojet engine aerothermodynamics.

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Related Institution

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Collaborative Innovation Center of Major Machine Manufacturing in Liaoning

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