Efficient Symplectic Integration of Satellite Orbits |
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Authors: | Seppo Mikkola |
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Institution: | (1) National Astronomical Observatory, Mitaka, Tokyo 181, Japan |
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Abstract: | The use of the extended phase space and time transformations for constructing efficient symplectic methods for computing the
long term behavior of perturbed two‐body systems are discussed. Main applications are for artificial satellite orbits. The
methods suggested here are efficient also for large eccentricities.
This revised version was published online in July 2006 with corrections to the Cover Date. |
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Keywords: | symplectic integration satellite orbits |
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