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永磁悬浮平台的分散串级控制方法

赵川 孙凤 裴文哲 金俊杰 徐方超 张晓友

赵川, 孙凤, 裴文哲, 金俊杰, 徐方超, 张晓友. 永磁悬浮平台的分散串级控制方法[J]. 西南交通大学学报, 2022, 57(3): 618-626. doi: 10.3969/j.issn.0258-2724.20210960
引用本文: 赵川, 孙凤, 裴文哲, 金俊杰, 徐方超, 张晓友. 永磁悬浮平台的分散串级控制方法[J]. 西南交通大学学报, 2022, 57(3): 618-626. doi: 10.3969/j.issn.0258-2724.20210960
ZHAO Chuan, SUN Feng, PEI Wenzhe, JIN Junjie, XU Fangchao, ZHANG Xiaoyou. Independent Cascade Control Method for Permanent Magnetic Levitation Platform[J]. Journal of Southwest Jiaotong University, 2022, 57(3): 618-626. doi: 10.3969/j.issn.0258-2724.20210960
Citation: ZHAO Chuan, SUN Feng, PEI Wenzhe, JIN Junjie, XU Fangchao, ZHANG Xiaoyou. Independent Cascade Control Method for Permanent Magnetic Levitation Platform[J]. Journal of Southwest Jiaotong University, 2022, 57(3): 618-626. doi: 10.3969/j.issn.0258-2724.20210960

永磁悬浮平台的分散串级控制方法

doi: 10.3969/j.issn.0258-2724.20210960
基金项目: 国家自然科学基金(52005345,52005344);国家重点研发计划(2020YFC2006701);辽宁省教育厅科学技术研究项目(LFGD2020002,LJGD 2019011);辽宁省“兴辽英才”计划 (XLYC1802077,XLYC1905003);辽宁省重点实验室建设项目(2020JH6/10500048)
详细信息
    作者简介:

    赵川(1993—),男,博士研究生,研究方向为永磁悬浮传送技术、电磁-永磁混合悬浮及其零功率控制,E-mail:zhaochuan@smail.sut.edu.cn

    通讯作者:

    金俊杰(1982—),女,副教授,博士,研究方向为永磁悬浮系统及其控制方法、机械系统多元驱动及其控制技术、多自由度磁力驱动器在先进加工设备中的应用等,E-mail:jinjunjie@sut.edu.cn

  • 中图分类号: TP271.4

Independent Cascade Control Method for Permanent Magnetic Levitation Platform

  • 摘要:

    针对各悬浮单元磁力特性差异导致的倾斜问题,设计一种用于无接触传送的永磁悬浮平台,提出了具有气隙偏差积分反馈的分散式串级控制方法. 首先,分析了悬浮平台的动力学模型与平衡条件,获得各悬浮单元气隙与平台三自由度之间的变换关系;其次,根据悬浮单元系统特点设计了双闭环串级控制系统,外环是以气隙为被控对象的主调节回路,内环是以转角为被控对象的随动回路,并引入气隙偏差进行积分反馈;最后,通过悬浮实验进行验证. 结果表明:引入积分反馈后,起浮后各磁悬浮单元气隙一致,向不同位置施加0.1 kg重物,各悬浮单元气隙同步增大0.12 mm;悬浮平台能够通过调节内环转角弥补磁力特性差异并实现偏载下水平悬浮,但系统的调节时间比无积分反馈的分散串级控制系统增加约1.4倍.

     

  • 图 1  永磁悬浮平台的三维模型

    Figure 1.  Three-dimensional model of permanent magnetic levitation platform

    图 2  永磁悬浮平台的运动分析简图

    Figure 2.  Schematic diagram of motion analysis for permanent magnetic levitation platform

    图 3  具有偏差积分反馈的分散串级控制系统框图

    Figure 3.  Block diagram of independent cascade control method with integral feedback of air gap deviation

    图 4  永磁悬浮平台的实验系统

    Figure 4.  Experimental system of permanent magnetic levitation platform

    图 5  无积分反馈时系统起浮实验结果

    Figure 5.  Experimental results during system floating without integral feedback

    图 6  有积分反馈时系统起浮实验结果

    Figure 6.  Experimental results during system floating with integral feedback

    图 7  4次加载位置示意(Ⅰ~ Ⅳ)

    Figure 7.  Schematic diagram of four loading positions (Ⅰ−Ⅳ)

    图 8  无积分反馈时在Ⅰ加载的实验结果

    Figure 8.  Experimental results of loading at position Ⅰ without integral feedback

    图 9  有积分反馈时在Ⅰ加载的实验结果

    Figure 9.  Experimental results of loading at position Ⅰ with integral feedback

    图 10  悬浮平台的气隙阶跃实验结果

    Figure 10.  Experimental results of air gap step for levitated platform

    表  1  施加偏载后悬浮系统的稳态气隙

    Table  1.   Steady-state air gap length of levitation system under eccentric load mm

    加载位置编号无气隙偏差补偿有气隙偏差补偿
    12341234
    03.943.924.114.174.004.004.004.00
    4.154.024.084.244.124.124.124.12
    4.054.164.214.114.124.124.124.12
    3.904.04.334.264.124.124.124.12
    4.003.874.204.394.124.124.124.12
    下载: 导出CSV

    表  2  施加偏载后永磁体的转角

    Table  2.   Rotational angle of permanent magnet under eccentric load (°)

    加载位置编号无气隙偏差补偿有气隙偏差补偿
    12341234
    059.552.955.259.158.456.353.159.6
    64.354.754.660.961.457.853.661.1
    61.957.457.057.760.458.654.559.7
    58.654.359.361.258.857.755.360.8
    60.951.957.064.260.256.254.461.9
    下载: 导出CSV
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出版历程
  • 收稿日期:  2021-11-15
  • 修回日期:  2022-03-13
  • 刊出日期:  2022-03-25

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