AN ALGORITHM OF SATELLITE INITIALIZATION ORBITAL CONFIRMATION

摘要：

Intercept satellite needs confirm its high precision orbit. The precision of satellite initialization orbit affects the precision of satellite final orbit directly. The general methods have low accuracy. This paper presents a spline function approximation method and uses it to confirm orbit. The method has more high accuracy and is easily operated. By simulation, this method could improve the orbit confirmation precision.

关键词： Intercept satellite Orbital confirmation Spline function approximation

作者: P.T.Wei G.Lei L.H.Sun X.Ma

作者单位: Xian Research Institute of High-tech, Xian, P. R. China

会议类型: 国际会议

会议名称: 2012 International Conference on System Simulation(2012年国际系统仿真学术会议)

会议地点: 上海

会议语种:英文

页码: 343-345

在线出版日期: 2012-04-06（万方平台首次上网日期，不代表论文的发表时间）