Explicit evolution relations with orbital elements for eccentric, inclined, elliptic and hyperbolic restricted few-body problems (2014)
Attributed to:
IoA Theoretical and X-ray Astronomy consolidation
funded by
STFC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1007/s10569-014-9537-8
Publication URI: http://dx.doi.org/10.1007/s10569-014-9537-8
Type: Journal Article/Review
Parent Publication: Celestial Mechanics and Dynamical Astronomy
Issue: 4