| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 5500376 | Physica D: Nonlinear Phenomena | 2016 | 20 Pages |
Abstract
As a possible application to astrodynamics, diffusing orbits as above can be used to design low cost maneuvers to change the inclination of an orbit of a satellite near L1 from a nearly-planar orbit to a tilted orbit with respect to the ecliptic. We explore different energy levels, and estimate the largest orbital inclination that can be achieved through our construction.
Related Topics
Physical Sciences and Engineering
Mathematics
Applied Mathematics
Authors
Amadeu Delshams, Marian Gidea, Pablo Roldan,