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https://github.com/gnss-sdr/gnss-sdr
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Remove unused variables
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@ -465,18 +465,6 @@ Gps_Ephemeris Gps_Navigation_Message::get_ephemeris() const
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ephemeris.alert_flag = b_alert_flag;
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ephemeris.antispoofing_flag = b_antispoofing_flag;
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// These parameters are empty; can be computed later with
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// ephemeris.sv_clock_drift(double transmitTime);
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// ephemeris.satellitePosition(double transmitTime);
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ephemeris.satClkDrift = d_satClkDrift;
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ephemeris.dtr = d_dtr;
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ephemeris.satpos_X = d_satpos_X;
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ephemeris.satpos_Y = d_satpos_Y;
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ephemeris.satpos_Z = d_satpos_Z;
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ephemeris.satvel_X = d_satvel_X;
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ephemeris.satvel_Y = d_satvel_Y;
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ephemeris.satvel_Z = d_satvel_Z;
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return ephemeris;
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}
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@ -195,22 +195,6 @@ private:
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int32_t i_Toa{}; // Almanac reference time [s]
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int32_t i_WN_A{}; // Modulo 256 of the GPS week number to which the almanac reference time (i_Toa) is referenced
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// clock terms
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// double d_master_clock{}; // GPS transmission time
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double d_dtr{}; // relativistic clock correction term
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double d_satClkDrift{};
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// satellite positions
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double d_satpos_X{}; // Earth-fixed coordinate x of the satellite [m]. Intersection of the IERS Reference Meridian (IRM) and the plane passing through the origin and normal to the Z-axis.
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double d_satpos_Y{}; // Earth-fixed coordinate y of the satellite [m]. Completes a right-handed, Earth-Centered, Earth-Fixed orthogonal coordinate system.
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double d_satpos_Z{}; // Earth-fixed coordinate z of the satellite [m]. The direction of the IERS (International Earth Rotation and Reference Systems Service) Reference Pole (IRP).
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// Satellite velocity
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double d_satvel_X{}; // Earth-fixed velocity coordinate x of the satellite [m]
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double d_satvel_Y{}; // Earth-fixed velocity coordinate y of the satellite [m]
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double d_satvel_Z{}; // Earth-fixed velocity coordinate z of the satellite [m]
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// satellite identification info
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int32_t i_channel_ID{};
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uint32_t i_satellite_PRN{};
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