气体活塞式压力计超局部化无模型自适应控制研究
DOI:
CSTR:
作者:
作者单位:

1.大连工业大学机械工程与自动化学院大连116034; 2.中国计量科学研究院北京100029

作者简介:

通讯作者:

中图分类号:

TH823.2TP273

基金项目:

国家重点研发计划(2024YFD2101102)项目资助


Research of ultra-local mode-free adaptive control for gas piston pressure gauge
Author:
Affiliation:

1.College of Mechanical Engineering and Automation, Dalian Polytechnic University, Dalian 116034, China; 2.National Institute of Metrology, Beijing 100029, China

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    活塞式压力计是一种重要的压力溯源检测装备。活塞系统是气体活塞式压力计的核心部件,由于气体介质特性,活塞精准定位和快速稳定是一项难题。通过分析气体活塞式压力计活塞系统的非线性因素,提出超局部化无模型自适应控制(ULMFAC)方法,采用超螺旋非奇异终端滑模控制(STNTSMC)与有限时间扰动观测器相结合,有效避免了滑模控制中的抖振现象,并显著提高了系统的动态响应特性。由于活塞有效面积、温度和介质泄漏等参数变化,基于超局部化无模型方法建立改进二阶动力学模型,避免基于模型的控制方法对于精确系统模型的约束。设计非奇异终端滑模面,解决了终端滑模控制中的奇异性问题,并利用自适应超螺旋方法抑制不连续控制引起的抖振现象,进一步提高系统的动态响应。构造扰动观测器估计系统的集总不确定性,实现有限时间稳定,通过Lyapunov函数证明了所设计控制方案的稳定性和有限时间收敛性。系统仿真和实验结果表明,ULMFAC方法在0.5、3和6 MPa的不同工况下,能够显著提高系统的鲁棒性、活塞的定位精度和动态响应,对于实现高精度和高效率的压力测量,具有重要的理论意义和实用价值。

    Abstract:

    The piston pressure gauge is a critical instrument for pressure traceability and measurement, with the piston system being its core component. Accurate positioning and rapid stabilization of the piston present significant challenges due to the properties of gas media. To address these challenges, a novel ultra-local mode-free adaptive control (ULMFAC) method is proposed, which analyzes the nonlinear characteristics of the piston system in gas piston pressure gauges. This method combines super-twisting nonsingular terminal sliding mode control (STNTSMC) with a finite-time disturbance observer, effectively preventing the chattering phenomenon typical of sliding mode control and greatly enhancing the system’s dynamic response. To account for parameter variations such as the effective piston area, temperature, and medium leakage, an improved second-order dynamics model is developed using an ultra-local model-free approach, eliminating the need for a precise system model, as required in model-based control methods. A nonsingular terminal sliding mode surface is designed to overcome singularity issues in terminal sliding mode control, while an adaptive supertwisting algorithm is applied to mitigate chattering and enhance system dynamics. A disturbance observer is used to estimate lumped uncertainties, ensuring finite-time stability. The stability and convergence of the proposed control scheme are confirmed through Lyapunov analysis. Simulations and experimental results demonstrate that the ULMFAC method significantly improves the robustness, piston positioning accuracy, and dynamic response speed under varying working conditions (0.5, 3 and 6 MPa). This method holds considerable theoretical importance and practical value for achieving high-precision and high-efficiency pressure measurements.

    参考文献
    相似文献
    引证文献
引用本文

庞桂兵,王思遥,高腾,杨远超,原浩.气体活塞式压力计超局部化无模型自适应控制研究[J].仪器仪表学报,2025,46(4):306-314

复制
相关视频

分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2025-06-23
  • 出版日期:
文章二维码