NUMERICAL SOLUTION OF SATELLITE MOTION UNDER THE EFFECTS OF THE EARTH’S GRAVITY OF THE AXIAL SYMMETRY AND DRAG FORCE IN TERMS OF THE KS-REGULARIZED VARIABLES | ||||
| Al-Azhar Bulletin of Science | ||||
| Article 31, Volume 2013, Issue 12, December 2013, Page 65-75 PDF (110.27 K) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/absb.2013.6586 | ||||
 View on SCiNiTO | ||||
| Author | ||||
| GAMAL F. ATTIA | ||||
| National Research Institute of Astronomy and Geophysics, Helwan, Egypt | ||||
| Abstract | ||||
| This paper is concerned with an orbit prediction using one of the best regular theories (KS-regularized variables). Perturbations due to the Earth’s gravitational field with axial symmetry up to the fourth order zonal harmonic and rotating/non-rotating atmosphere (variation in density model with height) are considered. Applications of the problem will be illustrated by numerical and graphical example. | ||||
| Keywords | ||||
| SATELLITE MOTION; THE EARTH’S GRAVITY; THE KS-REGULARIZED | ||||
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