Periodic solutions near the stationary steady motion of an artificial satellite in the normal gravitation field of the earth

Mathematics

Scientific paper

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Earth Gravitation, Earth Orbits, Gravitational Fields, Liapunov Functions, Orbit Calculation, Satellite Orbits, Equations Of Motion, Existence Theorems, Geopotential, Matrices (Mathematics), Periodic Functions, Power Series, Steady State

Scientific paper

The motion of a spherical artificial earth satellite traveling in the equatorial plane and subject to the normal gravitational field is considered. It is assumed that the perturbations which are not due to the earth's oblateness are small. The Liapunov-Siegel theorem is used to demonstrate the existence of two families of periodic solutions near the steady motion of the satellite. The solutions are presented in the form of d'Alembert series.

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