Annotation
A special perturbation function expansion in the three-body problem for orbital resonances in the case of large eccentricities is substantiated. The given expansion can be used to construct an analytical solution allowing the orbital evolution of asteroids and comets to be interpreted.
© 2016 Publisher M.V.Lomonosov Moscow State University
Authors
I.A. Gerasimov, B.R. Mushailov
Sternberg State Institute of Astronomy, Moscow State University, Leninskie Gory, Moscow, 119992, Russia
Sternberg State Institute of Astronomy, Moscow State University, Leninskie Gory, Moscow, 119992, Russia