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외란관측기를 이용한 비선형 자기부상 시스템의 제어 성능 향상

Control Performance Improvement of a Nonlinear Magnetic Levitation System with a Disturbance Observer

Journal of the Korean Society for Precision Engineering 2023;40(4):329-334.
Published online: April 1, 2023

1 숭실대학교 일반대학원 기계공학과

2 숭실대학교 기계공학부

1 Department of Mechanical Engineering, Graduate school, Soongsil University

2 School of Mechanical Engineering, Soongsil University

#E-mail: ahj123@ssu.ac.kr, TEL: +82-2-820-0654
• Received: November 11, 2022   • Revised: December 17, 2022   • Accepted: December 27, 2022

Copyright © The Korean Society for Precision Engineering

This is an Open-Access article distributed under the terms of the Creative Commons Attribution Non-Commercial License (http://creativecommons.org/licenses/by-nc/3.0) which permits unrestricted non-commercial use, distribution, and reproduction in any medium, provided the original work is properly cited.

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Citations

Citations to this article as recorded by  Crossref logo
  • Control Boost of a Magnetic Levitation System with Disturbance Observers
    Yupeng Zheng, Hyeong-Joon Ahn
    Journal of the Korean Society for Precision Engineering.2024; 41(4): 273.     CrossRef

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Control Performance Improvement of a Nonlinear Magnetic Levitation System with a Disturbance Observer
J. Korean Soc. Precis. Eng.. 2023;40(4):329-334.   Published online April 1, 2023
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J. Korean Soc. Precis. Eng.. 2023;40(4):329-334.   Published online April 1, 2023
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Control Performance Improvement of a Nonlinear Magnetic Levitation System with a Disturbance Observer
Image Image Image Image Image Image Image Image Image Image Image Image Image Image
Fig. 1 MLS [9] (Adapted from Ref. 9 on the basis of webpage)
Fig. 2 Open-loop frequency responses and closed-loop sensitivity functions of the MLS of different mass
Fig. 3 Control performances of the MLS W/O DOB in cases of different PID gains (upper: disturbance rejection and lower: command following)
Fig. 4 Schematic of the Simulink realtime block diagram of the MLS with DOB
Fig. 5 Simulink realtime block diagram of the MLS with DOB
Fig. 6 Disturbance rejection of the MLS with DOB of different τ
Fig. 7 Sensitivity function of the MLS with DOB of different τ
Fig. 8 Command following of MLS with DOB of different τ
Fig. 9 Disturbance rejection of the MLS with DOB against different disturbance frequencies
Fig. 10 Close-loop frequency responses of the MLS W/O and W/T DOB
Fig. 11 Disturbance rejection of the MLS of different masses W/T DOB
Fig. 12 Command following of the MLS with DOB for different command frequencies (mass = 32 g)
Fig. 13 Command following of the MLS of different masses W/T DOB (@1 Hz)
Fig. 14 Complementary sensitivity functions of the MLS W/O and W/T DOB
Control Performance Improvement of a Nonlinear Magnetic Levitation System with a Disturbance Observer

Parameters of MLS

Symbol Description Value
ci Leakage current 0.0243 [A]
fi Time constant of coil 0.0321 [s]
Fem P 1 Coil inductance 1.7521×10-2 [H]
Fem P 2 Coefficients of electromagnetic force 5.8231×10-3 [m]
ki Voltage-current static gain 2.6903 [A/V]
m Nominal mass of the steel ball 0.032 [kg]
x 10 Equilibrium position of the steel ball 0.01 [m]
x 30 Equilibrium current 0.6322 [A]

Disturbance rejection of the MLS with DOB of different τ

τ
[sec]
W/O DOB
[mm]
W/T DOB
[mm]
Rejection ratio
[%]
0.5 3.41 1.73 49.3
0.1 3.19 0.74 76.8
0.05 3.43 0.48 86.0

Disturbance rejection of the MLS against different frequencies

Freq.
[Hz]
W/O DOB
[mm]
W/T DOB
[mm]
Rejection ratio
[%]
0.5 1.89 0.31 83.6
1.0 4.07 0.63 84.5
1.5 2.91 1.01 65.3
2.0 2.35 1.54 34.5

Disturbance rejection of the MLS of different masses W/T DOB

Mass
[g]
W/O DOB
[mm]
W/T DOB
[mm]
Rejection ratio
[%]
19 3.08 0.62 79.9
32 4.12 0.62 85.0
39 5.75 0.56 90.3

Command following of the MLS with DOB for different command frequencies (mass = 32 g)

Freq. [Hz] Amp. ratio W/O DOB Amp. ratio W/T DOB
0.5 1.740 0.905
1.0 4.075 1.243
1.5 5.405 1.920

Command following of the MLS of different masses W/T DOB (@1 Hz)

Mass [g] Amp. ratio W/O DOB Amp. ratio W/T DOB
19 3.250 1.285
32 4.075 1.243
39 5.025 1.210
Table 1 Parameters of MLS
Table 2 Disturbance rejection of the MLS with DOB of different τ
Table 3 Disturbance rejection of the MLS against different frequencies
Table 4 Disturbance rejection of the MLS of different masses W/T DOB
Table 5 Command following of the MLS with DOB for different command frequencies (mass = 32 g)
Table 6 Command following of the MLS of different masses W/T DOB (@1 Hz)