Dynamics Analysis of Active Variable Stiffness Vibration Isolator for Whole-Spacecraft Systems Based on Nonlinear Output Frequency Response Functions
Crossref DOI link: https://doi.org/10.1007/s10338-020-00198-5
Published Online: 2020-11-05
Published Print: 2020-12
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Xu, Kefan
Zhang, Yewei http://orcid.org/0000-0003-1748-3849
Zhu, Yunpeng
Zang, Jian
Chen, Liqun
Funding for this research was provided by:
National Natural Science Foundation of China (11772205, 11902203)
Text and Data Mining valid from 2020-11-05
Version of Record valid from 2020-11-05
Article History
Received: 3 August 2020
Revised: 12 October 2020
Accepted: 14 October 2020
First Online: 5 November 2020