Rigid-flexible coupling dynamic modeling and vibration control for flexible spacecraft based on its global analytical modes
Crossref DOI link: https://doi.org/10.1007/s11431-017-9219-1
Published Online: 2018-10-19
Published Print: 2019-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Liu, Lun
Cao, DengQing
Wei, Jin
Text and Data Mining valid from 2018-10-19
Article History
Received: 19 October 2017
Accepted: 26 February 2018
First Online: 19 October 2018