Modeling and analysis of piezoelectric folded-beam isolator for attenuating micro-vibration in spacecraft.
发布时间：2025-04-30
点击次数：
- 发布时间：
- 2025-04-30
- 论文名称：
- Modeling and analysis of piezoelectric folded-beam isolator for attenuating micro-vibration in spacecraft.
- 发表刊物：
- International Journal of Computational Materials Science and Engineering
- 摘要：
- Design and modeling of anintelligentflexible isolation system for attenuating low-frequency micro-vibration are presented. The isolator consists of a payload platform, a supporting platformand four folded-beams withMFC(Macro Fiber Composite) actuators. In order to accurately analyze the system performance, a piezoelectric finite element model is built and validated by the modal analysis results derived from ANSYS. To widen the low-frequency isolation range for micro-vibration combinedwith modal frequency shift approach. the transfer functions of the active isolation system with different feedback control ways are derived based on the finite element model(FEM) model, in which the feedback signals can be absolute and relative accelerations, absolute and relative displacement, relative velocity, and mixed responses.
- 合写作者：
- Luo, Y., Zhang, Y., Zhang, X., Gao, X., Jia, K., & Xu, M., et al. (2018).
- 是否译文：
- 否
- 发表时间：
- 2018-03-13