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bugfix: Fixes signal identifier for GLONASS GNAV

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Signal identifier for GLONASS L1 C/A was changed internally to be `1G`
instead of the '1C' originally conceived from the navigation software.
Also, forces PRN number update from decoding interface
This commit is contained in:
Damian Miralles
2017-10-10 08:40:05 -06:00
parent e0dfd90916
commit ea675b4baa
6 changed files with 48 additions and 38 deletions
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36
src/algorithms/libs/rtklib/rtklib_conversions.cc
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@@ -71,24 +71,24 @@ geph_t eph_to_rtklib(const Glonass_Gnav_Ephemeris & glonass_gnav_eph)
gtime_t t_utc;
struct tm utcinfo;
rtklib_sat.sat = glonass_gnav_eph.i_satellite_slot_number; /* satellite number */
rtklib_sat.iode = glonass_gnav_eph.d_iode; /* IODE (0-6 bit of tb field) */
rtklib_sat.frq = glonass_gnav_eph.i_satellite_freq_channel; /* satellite frequency number */
rtklib_sat.svh = glonass_gnav_eph.d_l3rd_n; /* satellite health*/
rtklib_sat.sva = glonass_gnav_eph.d_F_T; /* satellite accuracy*/
rtklib_sat.age = glonass_gnav_eph.d_E_n; /* satellite age*/
rtklib_sat.pos[0] = glonass_gnav_eph.d_Xn*1000; /* satellite position (ecef) (m) */
rtklib_sat.pos[1] = glonass_gnav_eph.d_Yn*1000; /* satellite position (ecef) (m) */
rtklib_sat.pos[2] = glonass_gnav_eph.d_Zn*1000; /* satellite position (ecef) (m) */
rtklib_sat.vel[0] = glonass_gnav_eph.d_VXn*1000; /* satellite velocity (ecef) (m/s) */
rtklib_sat.vel[1] = glonass_gnav_eph.d_VYn*1000; /* satellite velocity (ecef) (m/s) */
rtklib_sat.vel[2] = glonass_gnav_eph.d_VZn*1000; /* satellite velocity (ecef) (m/s) */
rtklib_sat.acc[0] = glonass_gnav_eph.d_AXn*1000; /* satellite acceleration (ecef) (m/s^2) */
rtklib_sat.acc[1] = glonass_gnav_eph.d_AYn*1000; /* satellite acceleration (ecef) (m/s^2) */
rtklib_sat.acc[2] = glonass_gnav_eph.d_AZn*1000; /* satellite acceleration (ecef) (m/s^2) */
rtklib_sat.taun = glonass_gnav_eph.d_tau_n; /* SV clock bias (s) */
rtklib_sat.gamn = glonass_gnav_eph.d_gamma_n; /* SV relative freq bias */
rtklib_sat.age = glonass_gnav_eph.d_Delta_tau_n; /* delay between L1 and L2 (s) */
rtklib_sat.sat = glonass_gnav_eph.i_satellite_slot_number; /* satellite number */
rtklib_sat.iode = static_cast<int>(glonass_gnav_eph.d_t_b); /* IODE (0-6 bit of tb field) */
rtklib_sat.frq = glonass_gnav_eph.i_satellite_freq_channel; /* satellite frequency number */
rtklib_sat.svh = glonass_gnav_eph.d_l3rd_n; /* satellite health*/
rtklib_sat.sva = static_cast<int>(glonass_gnav_eph.d_F_T); /* satellite accuracy*/
rtklib_sat.age = static_cast<int>(glonass_gnav_eph.d_E_n); /* satellite age*/
rtklib_sat.pos[0] = glonass_gnav_eph.d_Xn*1000; /* satellite position (ecef) (m) */
rtklib_sat.pos[1] = glonass_gnav_eph.d_Yn*1000; /* satellite position (ecef) (m) */
rtklib_sat.pos[2] = glonass_gnav_eph.d_Zn*1000; /* satellite position (ecef) (m) */
rtklib_sat.vel[0] = glonass_gnav_eph.d_VXn*1000; /* satellite velocity (ecef) (m/s) */
rtklib_sat.vel[1] = glonass_gnav_eph.d_VYn*1000; /* satellite velocity (ecef) (m/s) */
rtklib_sat.vel[2] = glonass_gnav_eph.d_VZn*1000; /* satellite velocity (ecef) (m/s) */
rtklib_sat.acc[0] = glonass_gnav_eph.d_AXn*1000; /* satellite acceleration (ecef) (m/s^2) */
rtklib_sat.acc[1] = glonass_gnav_eph.d_AYn*1000; /* satellite acceleration (ecef) (m/s^2) */
rtklib_sat.acc[2] = glonass_gnav_eph.d_AZn*1000; /* satellite acceleration (ecef) (m/s^2) */
rtklib_sat.taun = glonass_gnav_eph.d_tau_n; /* SV clock bias (s) */
rtklib_sat.gamn = glonass_gnav_eph.d_gamma_n; /* SV relative freq bias */
rtklib_sat.age = static_cast<int>(glonass_gnav_eph.d_Delta_tau_n); /* delay between L1 and L2 (s) */
utcinfo.tm_mon = 0;
utcinfo.tm_mday = glonass_gnav_eph.d_N_T;