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基于动态系数法的微型涡喷发动机实时建模

徐鑫 张天宏 盛汉霖

中国机械工程Issue(2):243-246,247,5.
中国机械工程Issue(2):243-246,247,5.DOI:10.3969/j.issn.1004132X.2015.02.021

基于动态系数法的微型涡喷发动机实时建模

Research on MTE Real-time Modeling Based on Dynamic Coefficient Method

徐鑫 1张天宏 1盛汉霖1

作者信息

  • 1. 南京航空航天大学江苏省航空动力系统重点实验室,南京,210016
  • 折叠

摘要

Abstract

This paper obtained a series of rotating speed-fuel consumption steady state and dynamic property of the engine at some steady points by using system identification method of time domain, obtained steady state relationship and acceleration coefficient for full range by using interpolation method,and established real-time model of the engine for full range by using dynamic coefficient method.This model was characterized by simple structure,small calculating amount,high real-time control.Simulation results show that this model can well reflect the steady state and dynamic property of MTE,compared to experimental data,steady point’s deviation of the model is less than 1%,devia-tion of transient process is less than 6%,which can apply to fault-tolerant control of MTE.

关键词

微型涡喷发动机/容错控制/系统辨识/动态系数法/实时模型

Key words

micro-turbojet engine(MTE)/fault tolerant control/system identification/dynamic co-efficient method/real-time model

分类

航空航天

引用本文复制引用

徐鑫,张天宏,盛汉霖..基于动态系数法的微型涡喷发动机实时建模[J].中国机械工程,2015,(2):243-246,247,5.

基金项目

国家自然科学基金资助项目(51176075) (51176075)

江苏高校优势学科建设工程资助项目 ()

中国机械工程

OA北大核心CSCDCSTPCD

1004-132X

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