Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun–Earth circular restricted three-body problem
Crossref DOI link: https://doi.org/10.1007/s10569-014-9589-9
Published Online: 2014-10-05
Published Print: 2014-11
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Mingotti, G.
Sánchez, J. P.
McInnes, C. R.
Text and Data Mining valid from 2014-10-05