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
收藏
页码：275 / 285
页数：11
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