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Extrapolation and Fitting Algorithms for GLONASS Satellite Orbit

机译:GLONASS卫星轨道的外推和拟合算法

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The paper decoded the positioning data, received with GPS on6; GLONASS receiver of 24 channels (GG24 receiver), to get the orbit parameters of GLONASS satellites at first, and then took these data as initial value for the 4-order Runge-Kutta to orbit extrapolation and compared the extrapolation position with the position in broadcast ephemeris of GLONASS. The experiment indicates that the average positioning error of extrapolation position is less then 1.5 m. Meanwhile, it took Lagrange Interpolation and Chebyshev polynomials fitting these two methods to fitting the satellitesȁ9; orbit and compared with the extrapolation, the result indicates that the Chebyshev polynomials fitting could get a small error.
机译:论文解码了定位数据,并通过GPS开启接收6。 24通道GLONASS接收机(GG24接收机),首先获取GLONASS卫星的轨道参数,然后将这些数据作为4阶Runge-Kutta进行轨道外推的初始值,并将外推位置与广播位置进行比较GLONASS的星历。实验表明,外推位置的平均定位误差小于1.5 m。同时,采用拉格朗日插值和切比雪夫多项式拟合这两种方法来拟合卫星ȁ9。轨道并与外推法比较,结果表明Chebyshev多项式拟合可能会产生较小的误差。

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