摘要
推荐了一组对短、中、长积分间隔以及带耗散力或较大偏心率等多种类型卫星轨道数值积分皆可获取较高计算精度的线性多步积分公式 (MTM) 。
For solving the initial value problem of the particular second order ordinary differential equations y″=f(x,y) or y″+εy′=f(x,y) , a large number of linear multi step integration formulae have been constructed. A set of numerical integrators (Many Types Method), suitable to different integration intervals, are recommended.
出处
《天文学报》
CSCD
北大核心
2000年第4期434-439,共6页
Acta Astronomica Sinica
基金
中国科学院新疆分院院长择优基金!( 1 999)
关键词
卫星轨道
不同积分间隔
线性多步积分公式
satellite orbit, different integration intervals, linear multi step method