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ATMOSPHERIC DRAG PERTURBATION EFFECT ON THE SATELLITES ORBITS | ||
| Journal of University of Anbar for Pure Science | ||
| Article 13, Volume 2, Issue 2, 2008, Pages 62-72 PDF (1.69 M) | ||
| Document Type: Research Paper | ||
| DOI: 10.37652/juaps.2008.15315 | ||
| Author | ||
| Abdulh Rahman Hussain Salih* | ||
| Sciences of college/ University of Baghdad | ||
| Abstract | ||
| : In this paper the drag perturbation for the law orbit are studded ,Koll-method is suitable to used hear, equation of motion it's solved by numerical integration ;Rang-Kota-method was used ; to find the components of velocity and position and find the orbital parameters with perturbation .Study the effect of drag perturbation on the position , of satellite with time and on perigee , apogee , a ,e and age of satellite, Study the variation of satellite position and age with height we can increase the age of satellite to 40 times by increase the perigee height only 2 times, and by decrease A/m ratio and eccentricity also by rotate in the direction of the earth rotate. | ||
| Keywords | ||
| Atmospheric; Drag perturbation; satellites orbits | ||
| References | ||
|
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2- Chobotov,A.V.,1996, "Orbital Mechanics" ,American Institute of Aeronauties and Astronautics, Inc. Washington, Dc.USA.
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5- Anas Al-Hity,2002, "Orbital perturbation on the low Satellite orbit" M.Sc. thesis, Baghdad Univ.
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8-Monten, O. and Pfleger, D.T., 1994, 2-nd edition, company (springer-verlag), west Sussex po 208 nt, United Kingdom. | ||
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