Third-body perturbation effects on satellite orbit reduced to nonlinear system requiring elliptic integrals
The theory of long-term behavior of artificial satellite orbits due to third-body perturbations
1966-02-15
Report
No indication
English
The long-term prediction of artificial satellite orbits
AIAA | 1974
|Long-Term Evolution of Artificial Satellite Orbits Due to Resonant Tesseral Harmonics
Online Contents | 1996
|