基于卫星轨道特征的低轨卫星星历参数拟合法  

LEO SATELLITE EPHEMERIS PARAMETERS FITTING METHOD BASED ON ORBIT CHARACTER OF SATELLITE

作　　者：马开锋[1] 彭碧波[1] 洪樱[2] 

机构地区：[1]中国科学院测量与地球物理研究所 [2]武汉科技学院数理系,武汉430073

出　　处：《大地测量与地球动力学》2007年第1期85-90,共6页Journal of Geodesy and Geodynamics

基　　金：国家自然科学基金(40234039)

摘　　要：在分析低轨卫星轨道变化特征的基础上,考虑GPS广播星历参数的物理意义明确、生成速度快、精度高、参数少等特点,设计了一套适于低轨卫星在轨位置计算的星历参数,并对其算法进行了试算。同时对GPS广播星历15参数法与设计的25参数法进行了拟合对比,结果表明,同样条件下25参数法应用于低轨卫星轨道拟合时精度较高。On the basis of the orbit character of the LEO satellite and the advantages of definite physical meanings, quickly creating, high precision, fewer parameters of GPS broadcast ephemeris, a new sort of ephemeris parameters for calculating LEO satellite location is designed and analyzed through a example. Some significant comparisons are made between the 15-parameter method of GPS broadcast ephemeris and the designed 25-parameter method, the results show that the designed 25 parameters method has a higher precision for LEO satellite orbit fitting under the same condition.

关 键 词：GPS广播星历 低轨卫星 轨道分析 星历参数 拟合精度 

分 类 号：P227[天文地球—大地测量学与测量工程]