Long-term dynamic modeling of tethered spacecraft using nodal position finite element method and symplectic integration
Crossref DOI link: https://doi.org/10.1007/s10569-015-9640-5
Published Online: 2015-08-27
Published Print: 2015-12
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Li, G. Q.
Zhu, Z. H.
Funding for this research was provided by:
Natural Sciences and Engineering Research Council of Canada (503114)
National Natural Science Foundation of China (11372177)
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