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Error propagation characteristic analysis of halo orbit based on condition number of state transition matrix

Crossref DOI link: https://doi.org/10.1007/s10509-016-2856-3

Published Online: 2016-08-11

Published Print: 2016-09

Update policy: https://doi.org/10.1007/springer_crossmark_policy

Authors

Sun, Yu https://orcid.org/0000-0002-4765-3194
Zhang, Jin
Funding

Funding for this research was provided by:

National Natural Science Foundation of China (No.11402295)

Science Project of the National University of Defense Technology (No.JC14-01-05)
License Information

License valid from 2016-08-11