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基于复合控制的磁悬浮CMG动框架效应抑制

王舒 郑世强

王舒, 郑世强. 基于复合控制的磁悬浮CMG动框架效应抑制[J]. 北京航空航天大学学报, 2020, 46(12): 2339-2347. doi: 10.13700/j.bh.1001-5965.2019.0610
引用本文: 王舒, 郑世强. 基于复合控制的磁悬浮CMG动框架效应抑制[J]. 北京航空航天大学学报, 2020, 46(12): 2339-2347. doi: 10.13700/j.bh.1001-5965.2019.0610
WANG Shu, ZHENG Shiqiang. Composite control method for gimbal excitation effect suppression of magnetically suspended CMGs[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(12): 2339-2347. doi: 10.13700/j.bh.1001-5965.2019.0610(in Chinese)
Citation: WANG Shu, ZHENG Shiqiang. Composite control method for gimbal excitation effect suppression of magnetically suspended CMGs[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(12): 2339-2347. doi: 10.13700/j.bh.1001-5965.2019.0610(in Chinese)

基于复合控制的磁悬浮CMG动框架效应抑制

doi: 10.13700/j.bh.1001-5965.2019.0610
基金项目: 

国家自然科学基金 61822302

详细信息
    作者简介:

    王舒  女, 硕士研究生。主要研究方向:磁悬浮控制力矩陀螺磁轴承抗干扰控制技术

    郑世强  男, 博士, 副教授, 博士生导师。主要研究方向:航天器新型惯性执行机构、高速磁悬浮电机技术及应用

    通讯作者:

    郑世强, E-mail:zhengshiqiang@buaa.edu.cn

  • 中图分类号: TP273+.3

Composite control method for gimbal excitation effect suppression of magnetically suspended CMGs

Funds: 

National Nalural Science Foundation of China 61822302

More Information
  • 摘要:

    针对磁悬浮控制力矩陀螺(MSCMG)动框架效应导致转子悬浮精度和稳定性降低的问题,提出一种角加速率自适应前馈控制与自抗扰控制(ADRC)相结合的复合控制方法。建立了MSCMG转子动力学模型,分析了框架转动情况下的磁轴承扰动力矩,设计了角加速率自适应算法和线性扩张状态观测器,并结合状态反馈控制设计了复合控制器,同时对磁轴承控制系统进行了稳定性分析,仿真结果验证了所提复合控制方法的有效性。利用研制的样机搭建实验平台进行验证,结果表明:所提方法与传统PID控制方法相比,磁悬浮转子收敛后的位移峰峰值降低了39.6%,提高了磁悬浮系统的抗干扰能力。

     

  • 图 1  磁悬浮控制力矩陀螺示意图

    Figure 1.  Schematic diagram of MSCMG

    图 2  磁悬浮高速转子系统坐标图

    Figure 2.  System coordinate of magnetic levitation high-speed rotor

    图 3  MSCMG磁轴承复合控制方法原理框图

    Figure 3.  Principle block diagram for magnetic bearing composite control method of MSCMG

    图 4  自抗扰控制器结构

    Figure 4.  Structure diagram of active disturbance rejection controller

    图 5  角加速率自适应前馈控制框图

    Figure 5.  Block diagram of adaptive feedforward control module with angular acceleration rate

    图 6  复合控制下磁轴承系统根轨迹图

    Figure 6.  Root locus of magnetic bearing system with composite control method

    图 7  角加速率自适应算法权值波形

    Figure 7.  Weight value waveform of adaptive angular acceleration rate algorithm

    图 8  基于复合控制的转子位移波形

    Figure 8.  Rotor displacement waveform with composite control method

    图 9  MSCMG实验平台

    Figure 9.  Experimental setup of MSCMG

    图 10  基于PID控制的转子位移波形

    Figure 10.  Rotor displacement waveform with PID control method

    图 11  基于ADRC控制下的转子位移波形

    Figure 11.  Rotor displacement waveform with ADRC method

    图 12  复合控制下的转子位移波形

    Figure 12.  Rotor displacement waveform with composite control method

    表  1  MSCMG模型参数

    Table  1.   Model parameters of MSCMG

    参数 数值
    转子质量m/kg 16.7
    转子赤道转动惯量Jr/(kg·m2) 0.8286
    转子极转动惯量Jz/(kg·m2) 0.1302
    磁轴承中心到转子质心距离lm/m 0.0725
    传感器到转子质心距离ls/m 0.1110
    电流刚度ki/(N·A-1) 600
    位移刚度kh/(N·m-1) 2.4×106
    下载: 导出CSV

    表  2  磁轴承转子控制参数

    Table  2.   Control parameters of magnetic bearing rotor

    参数 数值
    比例系数Kp 3.7578
    积分系数Ki 261.2088
    微分系数Kd 0.0081
    控制器带宽ωc 220
    观测器带宽ωo 4000
    收敛因子μ 5×10-4
    下载: 导出CSV
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出版历程
  • 收稿日期:  2019-12-04
  • 录用日期:  2020-03-13
  • 网络出版日期:  2020-12-20

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