Orbit computations with the Eulerian topological regular elements with oblateness |
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| Authors: | Arm A. Sharaf |
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| Affiliation: | (1) Department of Engineering Mathematics and Physics, Faculty of Engineering, Cairo University, Egypt;(2) Present address: Department of Computer Science, Faculty of Science, King Abdulaziz University, Jeddah, Kingdom of Saudi Arabia |
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| Abstract: | In this paper, the Eulerian set of topological regular elements was utilized to develop an orbit computation package for the initial value problem for any conic motion of artificial satellites in the Earth's gravitational field with axial symmetry. Applications for the two types of short- and long-term predictions are considered. The numerical results proved the high efficiency and flexibility of the package. |
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