mirror of
https://github.com/gnss-sdr/gnss-sdr
synced 2024-12-14 12:10:34 +00:00
Remove unused variables
This commit is contained in:
parent
9af3e6c125
commit
08782a2085
@ -465,18 +465,6 @@ Gps_Ephemeris Gps_Navigation_Message::get_ephemeris() const
|
|||||||
ephemeris.alert_flag = b_alert_flag;
|
ephemeris.alert_flag = b_alert_flag;
|
||||||
ephemeris.antispoofing_flag = b_antispoofing_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;
|
return ephemeris;
|
||||||
}
|
}
|
||||||
|
|
||||||
|
@ -195,22 +195,6 @@ private:
|
|||||||
int32_t i_Toa{}; // Almanac reference time [s]
|
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
|
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
|
// satellite identification info
|
||||||
int32_t i_channel_ID{};
|
int32_t i_channel_ID{};
|
||||||
uint32_t i_satellite_PRN{};
|
uint32_t i_satellite_PRN{};
|
||||||
|
Loading…
Reference in New Issue
Block a user