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一种位置平滑且速度抗饱和的襟翼控制方法

邱岳恒 李来福 郑久寿 孙军帅

液压与气动2026,Vol.50Issue(1):11-21,11.
液压与气动2026,Vol.50Issue(1):11-21,11.DOI:10.11832/j.issn.1000-4858.2026.01.002

一种位置平滑且速度抗饱和的襟翼控制方法

A Flap Control Method with Position Smoothing and Velocity Anti-saturation

邱岳恒 1李来福 1郑久寿 2孙军帅3

作者信息

  • 1. 中国民航大学 电子信息与自动化学院,天津 300300
  • 2. 航空工业西安计算技术研究所,陕西 西安 710065
  • 3. 航空工业庆安集团有限公司,陕西 西安 710082
  • 折叠

摘要

Abstract

The flap system's rapid response is prone to speed loop overshoot,which degrades system stability and shortens equipment life.To address this,a composite control method featuring"speed loop adaptive control and position loop smooth planning"is proposed.Firstly,a dynamic model of the flap system is constructed through an in-depth analysis of its components'working principles.Secondly,a theoretical mathematical model of the system under a loading environment is established to accurately characterize its dynamic behavior under actual operating conditions.Finally,to ensure stability and reduce start-up overshoot,the dynamic performance of the composite method is compared with traditional PID control in the speed loop.Based on the system performance specifications,the position loop performance of the composite control method is comprehensively verified under both no-load and load conditions.Simulation results demonstrate that,compared to the traditional PID control,the proposed method effectively reduces start-up overshoot,suppresses oscillation,and enhances system stability while meeting the system's rapidity requirements.

关键词

襟翼/动力驱动装置/自适应/平滑规划/加载环境

Key words

flap/power drive unit/adaptive/smooth planning/loading environment

分类

机械制造

引用本文复制引用

邱岳恒,李来福,郑久寿,孙军帅..一种位置平滑且速度抗饱和的襟翼控制方法[J].液压与气动,2026,50(1):11-21,11.

基金项目

国家重点研发计划(2022YFB4301003) (2022YFB4301003)

液压与气动

1000-4858

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