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基于ADRC和模型预测控制的直驱伺服阀振荡抑制研究

任鹏达 张伟 谢志刚 王彬

航空科学技术2024,Vol.35Issue(2):92-99,8.
航空科学技术2024,Vol.35Issue(2):92-99,8.DOI:10.19452/j.issn1007-5453.2024.02.011

基于ADRC和模型预测控制的直驱伺服阀振荡抑制研究

Research on Spool Vibration Suppression of Direct Drive Servo Valve Based on ADRC and MPC

任鹏达 1张伟 2谢志刚 2王彬3

作者信息

  • 1. 南京航空航天大学,江苏 南京 210016
  • 2. 航空工业西安飞行自动控制研究所,陕西 西安 710076
  • 3. 南京航空航天大学,江苏 南京 210016||江苏省航空动力系统重点实验室,江苏 南京 210016
  • 折叠

摘要

Abstract

Direct drive servo valve gradually expands its application scenarios because of its advantages such as simple structure,strong antipollution ability and large output power.As one of the key components of flight control system,the characteristics and reliability of electro-hydraulic servo valve are directly related to flight performance and safety.In order to solve the problem of spool oscillation of a type of dual-system direct drive servo valve for aviation,a new control method for spool oscillation suppression is proposed in this paper.The component level mathematical model of the direct drive servo valve system is established,and the calculation is combined with the sudden fluid flow force model in the previous study.The composite control method of ADRC and active prediction is designed and compared with the traditional PID control method.The results show that the combined control method of ADRC and active prediction can effectively counteract the influence of sudden fluid flow force on the spool movement of linear motor current,and provide a theoretical reference for the controller design of direct drive servo valve under complex stress environment.

关键词

双系统直驱伺服阀/自抗扰控制器/模型预测控制/阀芯振荡/突变液流力

Key words

dual-system direct drive servo valve/ADRC/MPC/spool oscillation/sudden fluid flow force

分类

航空航天

引用本文复制引用

任鹏达,张伟,谢志刚,王彬..基于ADRC和模型预测控制的直驱伺服阀振荡抑制研究[J].航空科学技术,2024,35(2):92-99,8.

基金项目

航空科学基金(201907052001)Aeronautical Science Foundation of China(201907052001) (201907052001)

航空科学技术

1007-5453

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