Studies on global analytical mode for a three-axis attitude stabilized spacecraft by using the Rayleigh–Ritz method
Crossref DOI link: https://doi.org/10.1007/s00419-016-1155-3
Published Online: 2016-06-14
Published Print: 2016-12
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Liu, Lun
Cao, Dengqing
Tan, Xiaojun
Funding for this research was provided by:
National Natural Science Foundation of China (11472089)
License valid from 2016-06-14