Method for calculating GPS satellite position through broadcast ephemeris
A technology of broadcasting ephemeris and satellite positions, applied in the field of navigation and positioning, can solve problems such as occupying large memory and affecting calculation speed, and achieve the effect of improving accuracy and real-time performance
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[0026] A kind of method utilizing broadcast ephemeris to calculate GPS satellite position, comprises the steps:
[0027] Step 1: Calculate the coordinates of the satellite in the Cartesian coordinate system of the orbital plane;
[0028] 1a: Calculate the average angular velocity n of satellite motion, according to Kepler's third law, using the square root of the major semi-axis given in the broadcast ephemeris Calculate the average angular velocity n of TOE at the reference moment 0 , according to the perturbation parameter Δn given in the broadcast ephemeris, get n=n 0 +Δn;
[0029] 1b: Get the naturalized time t according to the GNSS time system k ;
[0030] 1c: Calculate the mean anomaly angle M of the satellite at the moment of observation k ,M k = M 0 +nt k ,M 0 the mean anomaly angle for the reference instant given for the broadcast ephemeris;
[0031] 1d: Calculate the apex angle E k ,E k = M k +esinE k , where e is the eccentricity of the satellite orbi...
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