The Integrated Flight/PropulsionController Design for a New Fighter

GUO Ying qing; TIAN Tong jun

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The Integrated Flight/PropulsionController Design for a New Fighter

更新时间：2026-07-07

- The Integrated Flight/PropulsionController Design for a New Fighter
- Vol. 18, Issue 4, Pages: 524-529(2003)
- 作者机构：
  
  西北工业大学航空动力与热力工程系,陕西,西安,710072
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2003
- 稿件说明：
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郭迎清, 田童军. 某新机综合飞行/推进系统H∞控制器设计[J]. 航空动力学报, 2003, 18(4): 524-529.

GUO Ying qing, TIAN Tong jun. The Integrated Flight/PropulsionController Design for a New Fighter[J]. 2003, 18(4): 524-529.
郭迎清, 田童军. 某新机综合飞行/推进系统H∞控制器设计[J]. 航空动力学报, 2003, 18(4): 524-529. DOI：

GUO Ying qing, TIAN Tong jun. The Integrated Flight/PropulsionController Design for a New Fighter[J]. 2003, 18(4): 524-529. DOI：

摘要

针对国内某新型战机及其装配的新型涡轮风扇发动机

本文研究了该综合飞行/推进系统一体化控制问题。首先建立了飞行子系统、推进子系统数学模型

在此基础上得到了飞行/推进系统综合模型;利用H∞混合灵敏度控制器设计方法

设计了综合系统控制器

对控制器设计中的一些关键问题作了讨论;最后通过仿真

表明所设计的综合控制系统具有较好的性能。

Abstract

The integrated flight/propulsion control system of a new fighter and its new turbofan engine are studied in this paper.Firstly

the models for the flight sub system and propulsion sub system are proposed

and then the model for integrated flight/propulsion system is set up.Secondly

the integrated flight/propulsion controller is designed based on the hybrid sensitivity approach;some key problems in controller design are discussed.Finally

the simulation results indicate that the designed integrated controller has good performances.

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Related Institution

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