Analysis and Experiment of 5-DOF Decoupled Spherical Vernier-Gimballing Magnetically Suspended Flywheel (VGMSFW)
Due to the capacity of outputting both the high precision torque and the instantaneous large torque, the vernier-gimballing magnetically suspended flywheel (VGMSFW) is regarded as the key actuator for spacecraft. In this paper, a 5-DOF active VGMSFW is presented. The 3-DOF translation and 2-DOF defl...
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IEEE
2020-01-01
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Online Access: | https://ieeexplore.ieee.org/document/9112204/ |
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author | Qiang Liu Heng Li Wei Wang Cong Peng Zengyuan Yin |
author_facet | Qiang Liu Heng Li Wei Wang Cong Peng Zengyuan Yin |
author_sort | Qiang Liu |
collection | DOAJ |
description | Due to the capacity of outputting both the high precision torque and the instantaneous large torque, the vernier-gimballing magnetically suspended flywheel (VGMSFW) is regarded as the key actuator for spacecraft. In this paper, a 5-DOF active VGMSFW is presented. The 3-DOF translation and 2-DOF deflection motions of the rotor are respectively realized by the spherical magnetic resistance magnetic bearings and the Lorentz magnetic bearing. The mathematical model of the deflection torque is established, and the decoupling between the 2-DOF deflections is demonstrated by the numerical analysis method. Compared with the conventional cylindrical magnetic bearings-rotor system, the spherical system is proven to eliminate the coupling between the rotor translation and deflection. In addition, a set of spherical magnetic resistance magnetic bearings with six-channel decoupling magnetic circuit are adopted to achieve the 3-DOF translation decoupling. The rotor dynamic model is derived, and the control system is established. The decoupling experiments and the torque experiments of the prototype are carried out. The results show that the decoupling among 5-DOF motions is realized and the instantaneous large torque can be obtained, which indicates that the requirements of the spacecraft can be highly satisfied by the spherical VGMSFW. |
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language | English |
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spelling | doaj.art-3d5f4f11c0df40e68c4d6f5ec3dd37ab2022-12-21T17:14:24ZengIEEEIEEE Access2169-35362020-01-01811170711171710.1109/ACCESS.2020.30011449112204Analysis and Experiment of 5-DOF Decoupled Spherical Vernier-Gimballing Magnetically Suspended Flywheel (VGMSFW)Qiang Liu0https://orcid.org/0000-0003-0310-3454Heng Li1https://orcid.org/0000-0003-2193-7030Wei Wang2https://orcid.org/0000-0002-4116-2319Cong Peng3https://orcid.org/0000-0001-9380-1410Zengyuan Yin4https://orcid.org/0000-0002-3225-7842Institute of Precision Electromagnetic Equipment and Advanced Measurement Technology, Beijing Institute of Petrochemical Technology, Beijing, ChinaInstitute of Precision Electromagnetic Equipment and Advanced Measurement Technology, Beijing Institute of Petrochemical Technology, Beijing, ChinaInstitute of Precision Electromagnetic Equipment and Advanced Measurement Technology, Beijing Institute of Petrochemical Technology, Beijing, ChinaCollege of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, ChinaDepartment of Aerospace Science and Technology, Space Engineering University, Beijing, ChinaDue to the capacity of outputting both the high precision torque and the instantaneous large torque, the vernier-gimballing magnetically suspended flywheel (VGMSFW) is regarded as the key actuator for spacecraft. In this paper, a 5-DOF active VGMSFW is presented. The 3-DOF translation and 2-DOF deflection motions of the rotor are respectively realized by the spherical magnetic resistance magnetic bearings and the Lorentz magnetic bearing. The mathematical model of the deflection torque is established, and the decoupling between the 2-DOF deflections is demonstrated by the numerical analysis method. Compared with the conventional cylindrical magnetic bearings-rotor system, the spherical system is proven to eliminate the coupling between the rotor translation and deflection. In addition, a set of spherical magnetic resistance magnetic bearings with six-channel decoupling magnetic circuit are adopted to achieve the 3-DOF translation decoupling. The rotor dynamic model is derived, and the control system is established. The decoupling experiments and the torque experiments of the prototype are carried out. The results show that the decoupling among 5-DOF motions is realized and the instantaneous large torque can be obtained, which indicates that the requirements of the spacecraft can be highly satisfied by the spherical VGMSFW.https://ieeexplore.ieee.org/document/9112204/VGMSFWspherical magnetic resistance magnetic bearingLorentz magnetic bearing5-DOF decoupled |
spellingShingle | Qiang Liu Heng Li Wei Wang Cong Peng Zengyuan Yin Analysis and Experiment of 5-DOF Decoupled Spherical Vernier-Gimballing Magnetically Suspended Flywheel (VGMSFW) IEEE Access VGMSFW spherical magnetic resistance magnetic bearing Lorentz magnetic bearing 5-DOF decoupled |
title | Analysis and Experiment of 5-DOF Decoupled Spherical Vernier-Gimballing Magnetically Suspended Flywheel (VGMSFW) |
title_full | Analysis and Experiment of 5-DOF Decoupled Spherical Vernier-Gimballing Magnetically Suspended Flywheel (VGMSFW) |
title_fullStr | Analysis and Experiment of 5-DOF Decoupled Spherical Vernier-Gimballing Magnetically Suspended Flywheel (VGMSFW) |
title_full_unstemmed | Analysis and Experiment of 5-DOF Decoupled Spherical Vernier-Gimballing Magnetically Suspended Flywheel (VGMSFW) |
title_short | Analysis and Experiment of 5-DOF Decoupled Spherical Vernier-Gimballing Magnetically Suspended Flywheel (VGMSFW) |
title_sort | analysis and experiment of 5 dof decoupled spherical vernier gimballing magnetically suspended flywheel vgmsfw |
topic | VGMSFW spherical magnetic resistance magnetic bearing Lorentz magnetic bearing 5-DOF decoupled |
url | https://ieeexplore.ieee.org/document/9112204/ |
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