摘要
对二体问题的状态传播问题, 以Ajisai 卫星某历元的初轨为例,考虑5d ( 天) 、10d ( 天) 和100d ( 天) 间隔的弧长, 本文分别给出了它们的分析解和数值解。结果表明: 对应于5d、10d、100d 间隔的弧长, 二体问题状态转移的分析解与数值解在10-10 、10 -8 和10-7 以内的相对偏差下能够保持其一致性。
The analytic and numerical solutions of state transition matrices of Two Body problem are presented in this paper. During the computation, a specific initial state vector of the satellite Ajisai is adopted and the time spans are 5 days, 10 days and 100days, respectively. The results indicate, at least, that analytic and numerical solutions agree with each other as long as the tolerances of their relative deviation of 10 -10 , 10 -8 and 10 -7 are acceptable,corresponding to the cases of 5 day, 10 day and 100 day intervals respectively.
出处
《云南天文台台刊》
CSCD
1999年第4期19-29,共11页
Publications of the Yunnan Observatoty
关键词
二体问题
状态转移
分析解
数值解
矩阵
two body problem
state transition
transition
analytic solution
numerical solution