• 中国计算机学会会刊
  • 中国科技核心期刊
  • 中文核心期刊

J4 ›› 2011, Vol. 33 ›› Issue (5): 171-176.

• 论文 • 上一篇    下一篇

星载GPS非差运动学定轨中的观测数据加权策略研究

谷德峰,易东云   

  1. (国防科学技术大学理学院,湖南 长沙 410073)
  • 收稿日期:2009-01-13 修回日期:2009-04-30 出版日期:2011-05-25 发布日期:2011-05-25
  • 作者简介:谷德峰(1980),男,辽宁东港人,博士,讲师,研究方向为现代统计方法和编队飞行的状态测量。易东云(1965),男,湖南株洲人,博士,教授,博士生导师,研究方向为动态系统分析和数据处理。
  • 基金资助:

    国防预研基金项目(9140A22040508KG01);航天支撑技术基金项目(2006HTGFKD)

Research on an Observations Weighing Method for Onboard GPS ZeroDifferential Kinematic Orbit Determination

GU Defeng,YI Dongyun   

  1. (School of Sciences,National University of Defense Technology,Changsha 410073,China)
  • Received:2009-01-13 Revised:2009-04-30 Online:2011-05-25 Published:2011-05-25

摘要:

星载GPS非差运动学定轨结果容易受到观测数据质量的影响,相位观测噪声远远小于伪码,如果将两种观测数据等权处理,会降低相位信息在参数解算中的作用;相位观测存在模糊,单独使用会导致参数估计结构不稳定;伪码观测噪声与接收天线高度角存在很强的相关性。本文根据星载GPS伪码和相位联合非差运动学定轨原理,结合GPS观测数据质量分析结果,提出了一种合理的加权策略,提高了星载GPS非差运动学定轨的精度和稳定性。对一个星期的CHAMP的观测数据进行处理,将非差运动学定轨结果与GFZ事后科学轨道进行对比,结果表明二者在R、T、N分量上差值的均方根为20cm、12cm、13cm,三维点位误差的均方根为27cm。通过分析多种不同加权策略的定轨精度差异,验证了本文提出的加权策略的有效性。

关键词: 星载GPS, 非差, 运动学定轨, 加权

Abstract:

Onboard GPS zerodifferential kinematic orbit determination is sensitive to the observation quality. The GPS phase noise is much less than the code noise. If both the observations are equally weighed, the parameter solution performance of the highly precise phase will be decreased. However, the phase observations have ambiguity, using phase observations signally will make the structure of parameter estimation unstable. And the code noise has significant correlation with receiving antenna elevation. The GPS observation quality is analyzed. Combining the analyzed results with the principle of zerodifferential kinematic orbit determination based on code and phase, a reasonable weighing method is proposed, and the precision and stability of onboard GPS zerodifferential kinematic orbit determination is improved. Observations on the CHAMP satellite for one week are tested. The zerodifferential kinematic orbit determination results are compared with the GFZ science orbit. The RMSs (root of mean square) in the R, T and N components are 20cm, 12cm and 13cm, and the RMS in the threedimension is 27cm. The precision comparison of several different weighing methods for orbit determination shows that the proposed weighing method is efficient.

Key words: onboard GPS;zerodifferential;kinematic orbit determination;weighing