Ejection-collision orbits with the more massive primary in the planar elliptic restricted three body problem Conxita Pinyol OriginalPaper Pages: 315 - 331
Infinitesimal orbits around lagrange points in the elliptic, restricted three-body problem Dan ŞelaruCătălin Cucu-Dumitrescu OriginalPaper Pages: 333 - 346
Solutions homoclinic to regular precessions of a symmetric satellite Andrzej J. MaciejewskiKrzysztof Goźiewski OriginalPaper Pages: 347 - 368
Analytical linear perturbation theory for highly eccentric satellite orbits Eugene BrumbergVictor A. BrumbergMichael Soffel OriginalPaper Pages: 369 - 387
