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两种GPS广播星历参数算法的比较
  • 期刊名称:空间科学学报, 2006, 26(5): 382-387
  • 时间:0
  • 分类:V423.4[航空宇航科学与技术—飞行器设计;航空宇航科学技术]
  • 作者机构:[1]西安测绘研究所,西安710054
  • 相关基金:国家自然科学基金项目(40274002,40474001)和地球空间环境与大地测量教育部重点实验室开放研究基金项目(146999032423304-11)共同资助
  • 相关项目:自适应卫星定轨理论及应用
中文摘要:

介绍了新GPS广播星历参数,分析了新旧GPS广播星历参数及其用户算法的区别,导出了卫星位置矢量对新GPS广播星历参数的偏导数,并与IBGPS广播星历参数偏导数进行了简要的比较分析.计算结果表明,两种GPS广播星历参数算法都能很好地描述MEO卫星的轨道特性,且广播星历参数拟合算法的精度损失仅为数厘米.

英文摘要:

The precision, efficiency and reliability of GPS broadcast ephemeris parameter algorithms are remarkably important in the real-time kinematic GPS navigation and positioning. Two kinds of GPS broadcast ephemeris parameters and their user algorithms are introduced in the last GPS interface specification. In this paper, the two algorithms are compared to provide some reference for the broadcast ephemeris parameter research or design. Firstly the new GPS broadcast ephemeris parameters and their user algorithms are briefly introduced, and the differences between the new and old algorithms are analyzed and it is found that the distinctness of the two user algorithms is consistent with those of the broadcast ephemeris parameters. Then the partial derivatives of the satellite position vector to the new GPS broadcast ephemeris parameters are presented based on the calculated expression of the satellite position, which is compared with those of the old GPS broadcast ephemeris parameters. Finally a set of simulation data is used to test and compare the new and old GPS broadcast ephemeris parameter algorithms. Calculation results show that the orbit characters of the MEO satellite can be accurately described by the two kinds of GPS broadcast ephemeris parameters, and the precision losses of the two fitting algorithms are almost several centimeters.

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