Design and Research of Lorentz Force Magnetic Levitation Vibration Isolation Platform
To address the micro-vibration isolation requirements of precision payloads in spacecraft, a Lorentz force-based magnetic levitation series vibration isolation platform is proposed. The Lorentz force actuator, overall coupling characteristics, and low-frequency vibration isolation performance of the platform are optimized, simulated, and experimentally validated. During the actuator design phase, an equivalent magnetic circuit model and an equivalent current model are established for the planar actuator. The theoretical relationship between magnetic flux density in the air gap and magnetization length is derived. Through finite element simulation, the optimal magnetization length is determined to be 7 mm. For the coupling analysis, a dynamic model of the platform is developed to quantify the coupling effects between translational and rotational motions. To evaluate the low-frequency vibration isolation performance, sinusoidal displacement at various frequencies is applied to emulate the space vibration environment and validate the isolation capability. The results show that the platform has low translational-rotational cross-coupling, and the vibration transmissibility of low-frequency micro-vibration is less than 35 dB. This system offers a high-precision, low-coupling solution for vibration isolation in precision optical instruments.
Authors
- Baiqi Li (ORCID: https://orcid.org/0000-0002-2135-8656)
- Chunmiao Yu (ORCID: https://orcid.org/0000-0003-3285-2702)
- Weijie Wang (ORCID: https://orcid.org/0000-0001-7697-431X)
- Lifen Wang (ORCID: https://orcid.org/0000-0002-1628-0284)
- Yanxia Yang
Institutions
- Space Engineering University (CN)
Publication Details
- Journal
- Aerospace
- Published
- 2025-10-28
- DOI
- https://doi.org/10.3390/aerospace12110965
- Primary Topic
- Vibration Control and Rheological Fluids
- Type
- article
- Field-Weighted Citation Impact
- 0.00
Funders
- National Natural Science Foundation of China