Design and application of a disturbance rejection rotor speed control method for turbo-shaft engines

ZHANG Hai-bo; SUN Jian-guo; SUN Li-guo

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Design and application of a disturbance rejection rotor speed control method for turbo-shaft engines

更新时间：2026-07-07

- Design and application of a disturbance rejection rotor speed control method for turbo-shaft engines
- Vol. 25, Issue 4, (2010)
- 作者机构：
  
  南京航空航天大学能源与动力学院,南京,210016
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2010
- 稿件说明：
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ZHANG Hai-bo, SUN Jian-guo, SUN Li-guo. Design and application of a disturbance rejection rotor speed control method for turbo-shaft engines[J]. 2010, 25(4).
DOI：

ZHANG Hai-bo, SUN Jian-guo, SUN Li-guo. Design and application of a disturbance rejection rotor speed control method for turbo-shaft engines[J]. 2010, 25(4). DOI：

摘要

主要研究了涡轴发动机控制问题.自抗扰控制(ADRC)是近年来新兴的控制方法

在不改变原有发动机串级比例积分微分(PID)控制结构的基础上

提出并构建了一种串级PID+扭矩ADRC补偿的控制结构

该结构充分利用了ADRC控制强的干扰补偿能力.最后

在直升机/发动机综合模型仿真环境下

通过模拟直升机大幅急速升降操作

验证了该算法具有比较理想的抗扰控制效果

能够较好地抑制直升机操控过程中大的扭矩扰动对涡轴发动机造成的不利影响.

Abstract

Turbo-shaft engine's control methodology was mainly studied in this article.Active disturbance rejection control(ADRC) method has been emerging in recent years.A hybrid control structure

i.e.an cascade proportion integration differentiation(PID) combined with torque's ADRC compensation

was proposed to improve the engine's disturbance rejection ability

and keep the formal control structure of the engine unchanged.The control system takes advantage of the excellent strong disturbance compensation property.The control system has better dynamic disturbance rejection ability than traditional system by simulation of helicopter's rapid lifting up and down based on the integrated helicopter/ turbo shaft engine platform.

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Related Author

YAN Chang-kai

ZHOU Xiao

CHEN Guo-qian

ZHANG Hai-bo

YAN Chang-kai

WANG Jian-kang

ZHANG Hai-bo

YAO Wen-rong

Related Institution

College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics

China Aviation Motor Control System Institute, Aviation Industry Corporation of China

China Helicopter Research and Development Institute, Aviation Industry Corporation of China, Limited

National Laboratory of Science and Technology on Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics

北京航空航天大学航空科学与工程学院

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