mirrors/gnss-sdr
1
0
Fork 0
mirror of https://github.com/gnss-sdr/gnss-sdr synced 2025-04-08 19:56:46 +00:00
Code Issues Releases Wiki Activity

Fix typo

Browse Source
This commit is contained in:
Carles Fernandez 2019-08-17 14:26:11 +02:00
parent afc7f1031c
commit b2045076bd
No known key found for this signature in database
GPG Key ID: 4C583C52B0C3877D
1 changed files with 14 additions and 14 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

28
src/algorithms/libs/rtklib/rtklib_conversions.cc
View File

@ -77,7 +77,7 @@ obsd_t insert_obs_to_rtklib(obsd_t& rtklib_obs, const Gnss_Synchro& gnss_synchro
}
auto CN0_dB_Hz = static_cast<unsigned char>(std::round(CN0_dB_Hz_est / 0.25));
rtklib_obs.SNR[band] = CN0_dB_Hz;
//Galileo is the third satellite system for RTKLIB, so, add the required offset to discriminate Galileo ephemeris
// Galileo is the third satellite system for RTKLIB, so, add the required offset to discriminate Galileo ephemeris
switch (gnss_synchro.System)
{
case 'G':
@ -107,7 +107,7 @@ obsd_t insert_obs_to_rtklib(obsd_t& rtklib_obs, const Gnss_Synchro& gnss_synchro
rtklib_obs.sat = gnss_synchro.PRN;
}
// Mote that BeiDou week numbers do not need adjustment for foreseeable future. Consider change
// Note that BeiDou week numbers do not need adjustment for foreseeable future. Consider change
// to more elegant solution
// if(gnss_synchro.System == 'C')
// {
@ -122,7 +122,6 @@ obsd_t insert_obs_to_rtklib(obsd_t& rtklib_obs, const Gnss_Synchro& gnss_synchro
// account for the TOW crossover transitory in the first 18 seconds where the week is not yet updated!
if (gnss_synchro.RX_time < 18.0)
{
//p_time += boost::posix_time::seconds(604800);
rtklib_obs.time = timeadd(rtklib_obs.time, 604800);
}
@ -130,6 +129,7 @@ obsd_t insert_obs_to_rtklib(obsd_t& rtklib_obs, const Gnss_Synchro& gnss_synchro
return rtklib_obs;
}
geph_t eph_to_rtklib(const Glonass_Gnav_Ephemeris& glonass_gnav_eph, const Glonass_Gnav_Utc_Model& gnav_clock_model)
{
double week;
@ -174,7 +174,7 @@ eph_t eph_to_rtklib(const Galileo_Ephemeris& gal_eph)
{
eph_t rtklib_sat = {0, 0, 0, 0, 0, 0, 0, 0, {0, 0}, {0, 0}, {0, 0}, 0.0, 0.0, 0.0, 0.0, 0.0,
0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, {}, {}, 0.0, 0.0};
//Galileo is the third satellite system for RTKLIB, so, add the required offset to discriminate Galileo ephemeris
// Galileo is the third satellite system for RTKLIB, so, add the required offset to discriminate Galileo ephemeris
rtklib_sat.sat = gal_eph.i_satellite_PRN + NSATGPS + NSATGLO;
rtklib_sat.A = gal_eph.A_1 * gal_eph.A_1;
rtklib_sat.M0 = gal_eph.M0_1;
@ -185,8 +185,8 @@ eph_t eph_to_rtklib(const Galileo_Ephemeris& gal_eph)
rtklib_sat.i0 = gal_eph.i_0_2;
rtklib_sat.idot = gal_eph.iDot_2;
rtklib_sat.e = gal_eph.e_1;
rtklib_sat.Adot = 0; //only in CNAV;
rtklib_sat.ndot = 0; //only in CNAV;
rtklib_sat.Adot = 0; // only in CNAV;
rtklib_sat.ndot = 0; // only in CNAV;
rtklib_sat.week = adjgpsweek(gal_eph.WN_5); /* week of tow */
rtklib_sat.cic = gal_eph.C_ic_4;
@ -243,8 +243,8 @@ eph_t eph_to_rtklib(const Gps_Ephemeris& gps_eph)
rtklib_sat.i0 = gps_eph.d_i_0;
rtklib_sat.idot = gps_eph.d_IDOT;
rtklib_sat.e = gps_eph.d_e_eccentricity;
rtklib_sat.Adot = 0; //only in CNAV;
rtklib_sat.ndot = 0; //only in CNAV;
rtklib_sat.Adot = 0; // only in CNAV;
rtklib_sat.ndot = 0; // only in CNAV;
rtklib_sat.week = adjgpsweek(gps_eph.i_GPS_week); /* week of tow */
rtklib_sat.cic = gps_eph.d_Cic;
@ -301,14 +301,14 @@ eph_t eph_to_rtklib(const Beidou_Dnav_Ephemeris& bei_eph)
rtklib_sat.i0 = bei_eph.d_i_0;
rtklib_sat.idot = bei_eph.d_IDOT;
rtklib_sat.e = bei_eph.d_eccentricity;
rtklib_sat.Adot = 0; //only in CNAV;
rtklib_sat.ndot = 0; //only in CNAV;
rtklib_sat.Adot = 0; // only in CNAV;
rtklib_sat.ndot = 0; // only in CNAV;
rtklib_sat.svh = bei_eph.i_SV_health;
rtklib_sat.sva = bei_eph.i_SV_accuracy;
rtklib_sat.code = bei_eph.i_sig_type; /*B1I data*/
rtklib_sat.flag = bei_eph.i_nav_type; /*MEO/IGSO satellite*/
rtklib_sat.code = bei_eph.i_sig_type; /* B1I data */
rtklib_sat.flag = bei_eph.i_nav_type; /* MEO/IGSO satellite */
rtklib_sat.iode = static_cast<int32_t>(bei_eph.d_AODE); /* AODE */
rtklib_sat.iodc = static_cast<int32_t>(bei_eph.d_AODC); /* AODC */
@ -374,8 +374,8 @@ eph_t eph_to_rtklib(const Gps_CNAV_Ephemeris& gps_cnav_eph)
rtklib_sat.i0 = gps_cnav_eph.d_i_0;
rtklib_sat.idot = gps_cnav_eph.d_IDOT;
rtklib_sat.e = gps_cnav_eph.d_e_eccentricity;
rtklib_sat.Adot = gps_cnav_eph.d_A_DOT; //only in CNAV;
rtklib_sat.ndot = gps_cnav_eph.d_DELTA_DOT_N; //only in CNAV;
rtklib_sat.Adot = gps_cnav_eph.d_A_DOT; // only in CNAV;
rtklib_sat.ndot = gps_cnav_eph.d_DELTA_DOT_N; // only in CNAV;
rtklib_sat.week = adjgpsweek(gps_cnav_eph.i_GPS_week); /* week of tow */
rtklib_sat.cic = gps_cnav_eph.d_Cic;