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Remove unused variables

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This commit is contained in:
Carles Fernandez 2022-03-19 10:59:44 +01:00
parent 9af3e6c125
commit 08782a2085
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GPG Key ID: 4C583C52B0C3877D
2 changed files with 0 additions and 28 deletions
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12
src/core/system_parameters/gps_navigation_message.cc
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@ -465,18 +465,6 @@ Gps_Ephemeris Gps_Navigation_Message::get_ephemeris() const
ephemeris.alert_flag = b_alert_flag;
ephemeris.antispoofing_flag = b_antispoofing_flag;
// These parameters are empty; can be computed later with
// ephemeris.sv_clock_drift(double transmitTime);
// ephemeris.satellitePosition(double transmitTime);
ephemeris.satClkDrift = d_satClkDrift;
ephemeris.dtr = d_dtr;
ephemeris.satpos_X = d_satpos_X;
ephemeris.satpos_Y = d_satpos_Y;
ephemeris.satpos_Z = d_satpos_Z;
ephemeris.satvel_X = d_satvel_X;
ephemeris.satvel_Y = d_satvel_Y;
ephemeris.satvel_Z = d_satvel_Z;
return ephemeris;
}

16
src/core/system_parameters/gps_navigation_message.h
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@ -195,22 +195,6 @@ private:
int32_t i_Toa{}; // Almanac reference time [s]
int32_t i_WN_A{}; // Modulo 256 of the GPS week number to which the almanac reference time (i_Toa) is referenced
// clock terms
// double d_master_clock{}; // GPS transmission time
double d_dtr{}; // relativistic clock correction term
double d_satClkDrift{};
// satellite positions
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.
double d_satpos_Y{}; // Earth-fixed coordinate y of the satellite [m]. Completes a right-handed, Earth-Centered, Earth-Fixed orthogonal coordinate system.
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).
// Satellite velocity
double d_satvel_X{}; // Earth-fixed velocity coordinate x of the satellite [m]
double d_satvel_Y{}; // Earth-fixed velocity coordinate y of the satellite [m]
double d_satvel_Z{}; // Earth-fixed velocity coordinate z of the satellite [m]
// satellite identification info
int32_t i_channel_ID{};
uint32_t i_satellite_PRN{};