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Dynamics Analysis of Active Variable Stiffness Vibration Isolator for Whole-Spacecraft Systems Based on Nonlinear Output Frequency Response Functions

Published Online: 2020-11-05

Published Print: 2020-12

Authors

Xu, Kefan

Zhang, Yewei https://orcid.org/0000-0003-1748-3849
Zhu, Yunpeng

Zang, Jian

Chen, Liqun
Funding

Funding for this research was provided by:

National Natural Science Foundation of China (11772205)

National Natural Science Foundation of China (11902203)
License Information

Text and Data Mining valid from 2020-11-05

Version of Record valid from 2020-11-05
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Article History

Received: 3 August 2020

Revised: 12 October 2020

Accepted: 14 October 2020

First Online: 5 November 2020

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