Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
9506692 | Applied Mathematics and Computation | 2005 | 9 Pages |
Abstract
The present work deals with the encounter problem of two small masses m2 and m3 describing initially elliptical orbits around a massive oblate primary. The equations of motion are developed, up to the power 13 of the small parameter, both for the center of mass and for the relative motion of m2 and m3 without any restrictions on the orbital elements. The equations of motion of the center of mass are expressed in terms of the Struble variables.
Keywords
Related Topics
Physical Sciences and Engineering
Mathematics
Applied Mathematics
Authors
Mohamad Radwan, M.K. Ahmed, F.A. Abd El-Salam,