Infinitesimal orbits around lagrange points in the elliptic, restricted three-body problem

Autor:	Dan Şelaru, Catalin Cucu-Dumitrescu
Rok vydání:	1995
Předmět:	Applied Mathematics Infinitesimal Mathematical analysis Lagrangian point Astronomy and Astrophysics Orbital eccentricity Equilateral triangle Three-body problem Computational Mathematics Constraint algorithm Planar Space and Planetary Science Modeling and Simulation Mathematical Physics Mathematics
Zdroj:	Celestial mechanics and dynamical astronomy. 61:333-346
ISSN:	1572-9478 0923-2958
DOI:	10.1007/bf00049514
Popis:	This study presents a method of obtaining asymptotic approximations for motions near a Lagrange point in the planar, elliptic, restricted three-body problem by using a von Zeipel-type method. The calculations are carried out for a second-order escape solution in the proximity of the equilateral Lagrange point, L 4, where the primaries' orbital eccentricity is taken as the small parameter ɛ.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::f204e25f0186ca124feb19601c1f937e https://doi.org/10.1007/bf00049514 Zobrazit plný text záznamu Full text from SpringerLink