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https://github.com/gnss-sdr/gnss-sdr
synced 2025-01-29 02:14:51 +00:00
Modify CNAV message structure header
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@ -258,7 +258,10 @@ bool rtklib_solver::get_PVT(const std::map<int,Gnss_Synchro> & gnss_observables_
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//convert ephemeris from GNSS-SDR class to RTKLIB structure
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eph_data[valid_obs] = eph_to_rtklib(gps_cnav_ephemeris_iter->second);
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//convert observation from GNSS-SDR class to RTKLIB structure
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obsd_t newobs = {{0,0}, '0', '0', {}, {}, {}, {}, {}, {}};
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unsigned char default_code_ = static_cast<unsigned char>(CODE_NONE);
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obsd_t newobs = {{0,0}, '0', '0', {}, {},
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{default_code_, default_code_, default_code_},
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{}, {0.0, 0.0, 0.0}, {}};
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obs_data[valid_obs] = insert_obs_to_rtklib(newobs,
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gnss_observables_iter->second,
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gps_cnav_ephemeris_iter->second.i_GPS_week,
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@ -271,6 +274,53 @@ bool rtklib_solver::get_PVT(const std::map<int,Gnss_Synchro> & gnss_observables_
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DLOG(INFO) << "No ephemeris data for SV " << gnss_observables_iter->second.PRN;
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}
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}
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//GPS L5
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if(sig_.compare("5X") == 0)
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{
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gps_cnav_ephemeris_iter = gps_cnav_ephemeris_map.find(gnss_observables_iter->second.PRN);
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if (gps_cnav_ephemeris_iter != gps_cnav_ephemeris_map.cend())
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{
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// 1. Find the same satellite in GPS L1 band
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gps_ephemeris_iter = gps_ephemeris_map.find(gnss_observables_iter->second.PRN);
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if (gps_ephemeris_iter != gps_ephemeris_map.cend())
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{
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// 2. If found, replace the existing GPS L1 ephemeris with the GPS L5 ephemeris
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// (more precise!), and attach the L5 observation to the L1 observation in RTKLIB structure
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for (int i = 0; i < valid_obs; i++)
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{
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if (eph_data[i].sat == static_cast<int>(gnss_observables_iter->second.PRN))
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{
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eph_data[i] = eph_to_rtklib(gps_cnav_ephemeris_iter->second);
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obs_data[i] = insert_obs_to_rtklib(obs_data[i],
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gnss_observables_iter->second,
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gps_cnav_ephemeris_iter->second.i_GPS_week,
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2);//Band 3 (L5)
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break;
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}
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}
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}
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else
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{
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// 3. If not found, insert the GPS L5 ephemeris and the observation
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//convert ephemeris from GNSS-SDR class to RTKLIB structure
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eph_data[valid_obs] = eph_to_rtklib(gps_cnav_ephemeris_iter->second);
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//convert observation from GNSS-SDR class to RTKLIB structure
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unsigned char default_code_ = static_cast<unsigned char>(CODE_NONE);
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obsd_t newobs = {{0,0}, '0', '0', {}, {},
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{default_code_, default_code_, default_code_},
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{}, {0.0, 0.0, 0.0}, {}};
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obs_data[valid_obs] = insert_obs_to_rtklib(newobs,
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gnss_observables_iter->second,
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gps_cnav_ephemeris_iter->second.i_GPS_week,
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2);//Band 3 (L5)
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valid_obs++;
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}
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}
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else // the ephemeris are not available for this SV
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{
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DLOG(INFO) << "No ephemeris data for SV " << gnss_observables_iter->second.PRN;
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}
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}
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break;
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}
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default :
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@ -154,13 +154,13 @@ int gps_l5_telemetry_decoder_cc::general_work (int noutput_items __attribute__((
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//* delay by the formulae:
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//* \code
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//* symbolTime_ms = msg->tow * 6000 + *pdelay * 20
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d_TOW_at_current_symbol = static_cast<double>(msg.tow) * 6.0 + static_cast<double>(delay) * GPS_L5_PERIOD + 6 * GPS_L5_PERIOD;
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d_TOW_at_current_symbol = static_cast<double>(msg.tow) * 6.0 + static_cast<double>(delay) * GPS_L5i_PERIOD + 6 * GPS_L5i_PERIOD;
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d_TOW_at_current_symbol = floor(d_TOW_at_current_symbol * 1000.0) / 1000.0;
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d_flag_valid_word = true;
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}
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else
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{
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d_TOW_at_current_symbol += GPS_L5_PERIOD;
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d_TOW_at_current_symbol += GPS_L5i_PERIOD;
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if (current_synchro_data.Flag_valid_symbol_output == false)
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{
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d_flag_valid_word = false;
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@ -37,7 +37,7 @@
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#include <utility> // std::pair
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#include "MATH_CONSTANTS.h"
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#include "gnss_frequencies.h"
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#include "GPS_L2C.h"
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#include "GPS_L2C.h" // CNAV GPS NAVIGATION MESSAGE STRUCTURE
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// Physical constants
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const double GPS_L5_C_m_s = 299792458.0; //!< The speed of light, [m/s]
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@ -178,7 +178,7 @@ const int32_t GPS_L5q_INIT_REG[210] =
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const int GPS_L5_CNAV_DATA_PAGE_BITS = 300; //!< GPS L5 CNAV page length, including preamble and CRC [bits]
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const int GPS_L5_SYMBOLS_PER_BIT = 2;
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const int GPS_L5_SAMPLES_PER_SYMBOL = 1;
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const int GPS_L5_SAMPLES_PER_SYMBOL = 10;
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const int GPS_L5_CNAV_DATA_PAGE_SYMBOLS = 600;
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const int GPS_L5_CNAV_DATA_PAGE_DURATION_S = 6;
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