#include "SIM_config.h" #if AP_SIM_GPS_NMEA_ENABLED #include "SIM_GPS_NMEA.h" #include #include #include #include extern const AP_HAL::HAL& hal; using namespace SITL; /* formatted print of NMEA message, with checksum appended */ void GPS_NMEA::nmea_printf(const char *fmt, ...) { va_list ap; va_start(ap, fmt); char *s = nmea_vaprintf(fmt, ap); va_end(ap); if (s != nullptr) { write_to_autopilot((const char*)s, strlen(s)); free(s); } } /* send a new GPS NMEA packet */ void GPS_NMEA::publish(const GPS_Data *d) { struct timeval tv; struct tm *tm; char tstring[20]; char dstring[20]; char lat_string[20]; char lng_string[20]; simulation_timeval(&tv); tm = gmtime(&tv.tv_sec); // format time string hal.util->snprintf(tstring, sizeof(tstring), "%02u%02u%06.3f", tm->tm_hour, tm->tm_min, tm->tm_sec + tv.tv_usec*1.0e-6); // format date string hal.util->snprintf(dstring, sizeof(dstring), "%02u%02u%02u", tm->tm_mday, tm->tm_mon+1, tm->tm_year % 100); // format latitude double deg = fabs(d->latitude); hal.util->snprintf(lat_string, sizeof(lat_string), "%02u%08.5f,%c", (unsigned)deg, (deg - int(deg))*60, d->latitude<0?'S':'N'); // format longitude deg = fabs(d->longitude); hal.util->snprintf(lng_string, sizeof(lng_string), "%03u%08.5f,%c", (unsigned)deg, (deg - int(deg))*60, d->longitude<0?'W':'E'); nmea_printf("$GPGGA,%s,%s,%s,%01d,%02d,%04.1f,%07.2f,M,0.0,M,,", tstring, lat_string, lng_string, d->have_lock?1:0, d->have_lock?_sitl->gps_numsats[instance]:3, 1.2, d->altitude); const float speed_mps = d->speed_2d(); const float speed_knots = speed_mps * M_PER_SEC_TO_KNOTS; const auto ground_track_deg = degrees(d->ground_track_rad()); //$GPVTG,133.18,T,120.79,M,0.11,N,0.20,K,A*24 nmea_printf("$GPVTG,%.2f,T,%.2f,M,%.2f,N,%.2f,K,A", tstring, ground_track_deg, ground_track_deg, speed_knots, speed_knots * KNOTS_TO_METERS_PER_SECOND * 3.6); nmea_printf("$GPRMC,%s,%c,%s,%s,%.2f,%.2f,%s,,", tstring, d->have_lock?'A':'V', lat_string, lng_string, speed_knots, ground_track_deg, dstring); if (_sitl->gps_hdg_enabled[instance] == SITL::SIM::GPS_HEADING_HDT) { nmea_printf("$GPHDT,%.2f,T", d->yaw_deg); } else if (_sitl->gps_hdg_enabled[instance] == SITL::SIM::GPS_HEADING_THS) { nmea_printf("$GPTHS,%.2f,%c,T", d->yaw_deg, d->have_lock ? 'A' : 'V'); } else if (_sitl->gps_hdg_enabled[instance] == SITL::SIM::GPS_HEADING_KSXT) { // Unicore support // $KSXT,20211016083433.00,116.31296102,39.95817066,49.4911,223.57,-11.32,330.19,0.024,,1,3,28,27,,,,-0.012,0.021,0.020,,*2D nmea_printf("$KSXT,%04u%02u%02u%02u%02u%02u.%02u,%.8f,%.8f,%.4f,%.2f,%.2f,%.2f,%.2f,%.3f,%u,%u,%u,%u,,,,%.3f,%.3f,%.3f,,", tm->tm_year+1900, tm->tm_mon+1, tm->tm_mday, tm->tm_hour, tm->tm_min, tm->tm_sec, unsigned(tv.tv_usec*1.e-4), d->longitude, d->latitude, d->altitude, wrap_360(d->yaw_deg), d->pitch_deg, ground_track_deg, speed_mps, d->roll_deg, d->have_lock?1:0, // 2=rtkfloat 3=rtkfixed, 3, // fixed rtk yaw solution, d->have_lock?_sitl->gps_numsats[instance]:3, d->have_lock?_sitl->gps_numsats[instance]:3, d->speedE * 3.6, d->speedN * 3.6, -d->speedD * 3.6); } } #endif // AP_SIM_GPS_NMEA_ENABLED