ardupilot/libraries/SITL/SIM_GPS_NMEA.cpp

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#include "SIM_config.h"
#if AP_SIM_GPS_NMEA_ENABLED
#include "SIM_GPS_NMEA.h"
#include <SITL/SITL.h>
#include <AP_Common/NMEA.h>
#include <AP_HAL/AP_HAL.h>
2023-11-30 19:17:39 -04:00
#include <time.h>
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("$GPGGA,%s,%s,%s,%01d,%02d,%04.1f,%07.2f,M,0.0,M,,",
tstring,
lat_string,
lng_string,
d->have_lock?1:0,
d->have_lock?_sitl->gps_numsats[instance]:3,
1.2,
d->altitude);
const float speed_mps = d->speed_2d();
const float speed_knots = speed_mps * M_PER_SEC_TO_KNOTS;
const auto heading_rad = d->heading();
//$GPVTG,133.18,T,120.79,M,0.11,N,0.20,K,A*24
nmea_printf("$GPVTG,%.2f,T,%.2f,M,%.2f,N,%.2f,K,A",
tstring,
heading_rad,
heading_rad,
speed_knots,
speed_knots * KNOTS_TO_METERS_PER_SECOND * 3.6);
nmea_printf("$GPRMC,%s,%c,%s,%s,%.2f,%.2f,%s,,",
tstring,
d->have_lock?'A':'V',
lat_string,
lng_string,
speed_knots,
heading_rad,
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,
heading_rad,
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