Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1780653 | NRIAG Journal of Astronomy and Geophysics | 2013 | 5 Pages |
Abstract
In this paper, initial value problem for dynamical astronomy will be established using Bispherical coordinates. A computational algorithm is developed for the final state predictions for J2 gravity perturbed motion of the Earth’s artificial satellites. This algorithm is important in targeting, rendezvous maneuvers as well for scientific researches. The applications of the algorithm are illustrated by numerical examples of some test orbits of different eccentricities. The numerical results are extremely accurate and efficient.
Related Topics
Physical Sciences and Engineering
Physics and Astronomy
Astronomy and Astrophysics
Authors
M.A. Sharaf, H.H. Selim,