LEO星载GPS双向滤波定轨研究

GPS-Based Orbit Determination for LEO Using Bidirectional Filter

  • 摘要: 介绍了目前常用的LEO(low Earth orbiter)星载GPS定轨方法,分析了LEO星载GPS双向滤波定轨方法与其他几种主要定轨方法的区别。从卫星运动方程和星载GPS非差定轨观测方程出发,给出了LEO星载GPS双向滤波定轨方法的原理,采用自行研制的定轨软件对两颗GRACE(gravity recovery and climate ex-periment)卫星进行了定轨试验,通过与JPL(Jet Propulsion Laboratory)轨道的对比及KBR(-kband rangingsystem)观测数据的外部检核发现:①双向滤波定轨技术不仅能显著提高单向滤波开始阶段的定轨精度,而且可以从整体上提高卫星的定轨精度;②LEO星载GPS双向滤波定轨方法切实可行,相应的星载GPS定轨软件对GRACE卫星定轨精度在径向、沿轨方向和法向优于5 cm。

     

    Abstract: We analyzed the difference between bidirectional filter and other methods of precise orbit determination(POD) for LEO using GPS.The theory of GPS-based orbit determination for LEO using bidirectional filter was deduced from satellite motion equation and LEO GPS zero-differential(ZD) phase observation equation.Two GRACE satellites orbits were computed using the software developed by our institute.We compared results with the orbits provided by JPL and independently validated with k-band ranging(KBR) data.We found that POD using bidirectional filter improves not only the accuracy of individual filter result at the beginning of the data arc evidently,but also the accuracy of orbits in the whole data arc.We also found that the method of GPS-based orbit determination for LEO using bidirectional filter is feasible and the orbits of GRACE computed by the software are at a level of better than 5 cm in radial,transverse and normal direction,respectively.

     

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