The motion of axisymmetric satellite with drag and radiation pressure |
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| Authors: | S M Elshaboury A Mostafa |
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| Institution: | 1. Faculty of Science, Department of Mathematics, AinShams University, Cairo, Egypt
2. Department of Mathematics, German University of Cairo, Cairo, Egypt
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| Abstract: | The axisymmetric satellite problem including radiation pressure and drag is treated. The equations of motion of the satellite are derived. The energy-like and Laplace-like invariants of motion have been derived for a general drag force function of the polar angle, and the Laplace-like invariant is used to find the orbit equation in the case of a spherical satellite. Then using the small parameter, the orbit of the satellite is determined for an axisymmetric satellite. |
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