Efficient symplectic integration of satellite orbits

被引：12

作者：

Mikkola, S ^{[1
]}

机构：

[1] Natl Astron Observ, Tokyo 181, Japan

来源：

CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY | 1999年 / 74卷 / 04期

关键词：

symplectic integration; satellite orbits;

D O I：

10.1023/A:1008398121638

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

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.

引用

页码：275 / 285

页数：11

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