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Satellite Orbit Interpolation Algorithm Analysis for GNSS Terminals

机译:GNSS终端的卫星轨道插补算法分析

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Using real-time broadcast ephemeris to calculate satellite orbit information and clock parameters is an important calculation work in GNSS terminal positioning solution. Considering the development trend of GNSS terminal's low power consumption and Soc, the application and implementation of satellite orbit interpolation algorithm in GNSS receiver are analyzed. From the aspects of computing efficiency, application strategy and continuity, the performance of interpolation algorithm in GNSS real-time operation is analyzed. An implementation of GNSS satellite orbit interpolation algorithm is given to meet the needs of GNSS high frequency sub-location applications. The calculation results show that the method can fit the position and velocity parameter information of GNSS satellites orbit operation in real time. The satellite position accuracy is better than 1e-4 m and the velocity accuracy is better than le-3 m/s. It basically meets the requirements of high-frequency real-time calculation of GNSS receivers, and continuity.
机译:在GNSS终端定位解决方案中,使用实时广播星历来计算卫星轨道信息和时钟参数是一项重要的计算工作。结合GNSS终端低功耗和Soc的发展趋势,分析了卫星轨道插值算法在GNSS接收机中的应用与实现。从计算效率,应用策略和连续性等方面分析了插值算法在GNSS实时运算中的性能。给出了GNSS卫星轨道插值算法的实现方案,以满足GNSS高频子定位应用的需求。计算结果表明,该方法能够实时拟合GNSS卫星轨道运行的位置和速度参数信息。卫星定位精度优于1e-4 m,速度精度优于le-3 m / s。它基本满足GNSS接收机高频实时计算和连续性的要求。

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