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https://github.com/gnss-sdr/gnss-sdr
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Minor changes
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@@ -35,7 +35,7 @@ obsd_t insert_obs_to_rtklib(obsd_t & rtklib_obs, const Gnss_Synchro & gnss_synch
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{
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rtklib_obs.D[band] = gnss_synchro.Carrier_Doppler_hz;
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rtklib_obs.P[band] = gnss_synchro.Pseudorange_m;
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rtklib_obs.L[band] = gnss_synchro.Carrier_phase_rads / (2.0 * PI);
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rtklib_obs.L[band] = gnss_synchro.Carrier_phase_rads / PI_2;
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switch(band)
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{
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case 0:
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@@ -165,8 +165,6 @@ eph_t eph_to_rtklib(const Gps_Ephemeris & gps_eph)
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rtklib_sat.toc = gpst2time(rtklib_sat.week, toc);
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rtklib_sat.ttr = gpst2time(rtklib_sat.week, tow);
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//printf("EPHEMERIS TIME [%i]: %s,%f\n\r",rtklib_sat.sat,time_str(rtklib_sat.toe,3),rtklib_sat.toe.sec);
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return rtklib_sat;
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}
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@@ -183,7 +181,7 @@ eph_t eph_to_rtklib(const Gps_CNAV_Ephemeris & gps_cnav_eph)
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rtklib_sat.OMG0 = gps_cnav_eph.d_OMEGA0;
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// Compute the angle between the ascending node and the Greenwich meridian
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const double OMEGA_DOT_REF = -2.6e-9; // semicircles / s, see IS-GPS-200H pp. 164
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double d_OMEGA_DOT = OMEGA_DOT_REF * GPS_L2_PI + gps_cnav_eph.d_DELTA_OMEGA_DOT;
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double d_OMEGA_DOT = OMEGA_DOT_REF * PI + gps_cnav_eph.d_DELTA_OMEGA_DOT;
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rtklib_sat.OMGd = d_OMEGA_DOT;
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rtklib_sat.omg = gps_cnav_eph.d_OMEGA;
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rtklib_sat.i0 = gps_cnav_eph.d_i_0;
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