Third-order secular Solution of the variational equations of motion of a satellite in orbit around a non-spherical planet

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作者
M. K. Ammar
S. M. El Shaboury
M. R. Amin
机构
[1] Helwan University,Math. Dept. Fac. of Sci.
[2] Ain Shams University,Math. Dept. Fac. of Sci.
[3] National Research Center,Theoretical Physics Dept.
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关键词
Satellite earth orbit; Orbit Perturbation; Lagrange equations of motion; Earth oblateness; Secular variations;
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摘要
We constructed an analytical theory of satellite motion up to the third order relative to the oblateness parameter of the Earth (J2). Equations of secular variations was developed for the first three orbital elements (a, e, i) of an artificial satellite. The secular variations are solved in a closed form.
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页码:43 / 61
页数:18
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