Planar oscillation of a satellite in an elliptical orbit under the influence of solar radiation pressure and third body torque. I (Q1901611)
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scientific article; zbMATH DE number 817656
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Planar oscillation of a satellite in an elliptical orbit under the influence of solar radiation pressure and third body torque. I |
scientific article; zbMATH DE number 817656 |
Statements
Planar oscillation of a satellite in an elliptical orbit under the influence of solar radiation pressure and third body torque. I (English)
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16 November 1995
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By using Melnikov's method, the equations of motion are shown to be non- integrable. The radiation pressure has been taken to be of the order of the eccentricity \(e\) \((e\ll 1)\), and therefore the solution is obtained by using the BKM method for the non-resonance case. It is observed that the amplitude of the oscillation remains constant up to the second order of approximation.
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non-integrable equations of motions
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Melnikov's method
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eccentricity
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BKM method
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non-resonance case
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0.8625674247741699
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0.8428773880004883
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