Study of Aeroengine Adaptive Inverse Control

HU Wen-fei; HUANG Jin-quan

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Study of Aeroengine Adaptive Inverse Control

更新时间：2026-07-07

- Study of Aeroengine Adaptive Inverse Control
- Vol. 20, Issue 2, (2005)
- 作者机构：
  
  南京航空航天大学能源与动力学院,江苏,南京,210016
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2005
- 稿件说明：
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HU Wen-fei, HUANG Jin-quan. Study of Aeroengine Adaptive Inverse Control[J]. 2005, 20(2).
DOI：

HU Wen-fei, HUANG Jin-quan. Study of Aeroengine Adaptive Inverse Control[J]. 2005, 20(2). DOI：

摘要

将自适应逆控制方法应用于航空发动机控制系统中

用横向滤波器实现了发动机的建模和逆建模

设计了发动机转速自适应逆控制系统。针对系统存在的稳态误差

提出了带积分环节的发动机自适应逆控制结构

提高了系统的稳态精度。飞行包线内的数字仿真结果表明

自适应逆控制方案精度高、跟踪快、鲁棒性较强。

Abstract

The adaptive inverse control system for aeroengines was designed.The aeroengine was modeled using linear adaptive filters. The adaptive inverse control structure with integral control was proposed to reduce the steady-state error.Simulation of the aeroengine speed control system in the whole flight envelope was performed

and excellent tracking performance and robustness were obtained.

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Related Institution

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