总结了多年来构造适合卫星轨道计算的线性多步积分方法的研究进展;介绍了在构造积分公式的过 程中选取伪根的三条原则。结合具体算例,对推荐的适用于不同类型卫星轨道的五组线性多步积分公 式的性能与对称方法及科威尔方法作了详细地比对和评述。
Studies on Linear Multistep Algorithm for the Orbital Integration of Artificial Earth Satellites
Xu Jihong
(Urumqi Astronomical Observatory, The Chinese Academy of Sciences, Urumqi 830011)
(National Astronomical Observatories, The Chinese Academy of Sciences, Beijing 100012)
Abstract
The progress in my studies on linear multistep algorithm for the orbital integration of artificial earth satellites are summeried. Three basic principles are introduced to determine the spurious roots of the eigen-polynomial. Five linear multistep integrators are recommended to use in practice, and they have obvious advantages over both symmetric and Cowell methods by means of their comparisons each other.