Attitude stability of a spacecraft with two flexible solar arrays on a stationary orbit around an asteroid subjected to gravity gradient torque
Crossref DOI link: https://doi.org/10.1007/s10509-014-1863-5
Published Online: 2014-06-01
Published Print: 2014-06
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zhang, Ming-Jiang
Zhao, Chang-Yin
Text and Data Mining valid from 2014-06-01