void AP_ADSB::send_dynamic_out(const mavlink_channel_t chan)
{
const AP_GPS &gps = AP::gps();
const Vector3f &gps_velocity = gps.velocity();
const int32_t latitude = _my_loc.lat;
const int32_t longitude = _my_loc.lng;
const int32_t altGNSS = _my_loc.alt * 10; // convert cm to mm
const int16_t velVert = gps_velocity.z * 1E2; // convert m/s to cm/s
const int16_t nsVog = gps_velocity.x * 1E2; // convert m/s to cm/s
const int16_t ewVog = gps_velocity.y * 1E2; // convert m/s to cm/s
const uint8_t fixType = gps.status(); // this lines up perfectly with our enum
const uint8_t emStatus = 0; // TODO: implement this ENUM. no emergency = 0
const uint8_t numSats = gps.num_sats();
const uint16_t squawk = out_state.cfg.squawk_octal;
uint32_t accHoriz = UINT_MAX;
float accHoriz_f;
if (gps.horizontal_accuracy(accHoriz_f)) {
accHoriz = accHoriz_f * 1E3; // convert m to mm
}
uint16_t accVert = USHRT_MAX;
float accVert_f;
if (gps.vertical_accuracy(accVert_f)) {
accVert = accVert_f * 1E2; // convert m to cm
}
uint16_t accVel = USHRT_MAX;
float accVel_f;
if (gps.speed_accuracy(accVel_f)) {
accVel = accVel_f * 1E3; // convert m/s to mm/s
}
uint16_t state = 0;
if (out_state._is_in_auto_mode) {
state |= UAVIONIX_ADSB_OUT_DYNAMIC_STATE_AUTOPILOT_ENABLED;
}
if (!out_state.is_flying) {
state |= UAVIONIX_ADSB_OUT_DYNAMIC_STATE_ON_GROUND;
}
// TODO: confirm this sets utcTime correctly
const uint64_t gps_time = gps.time_epoch_usec();
const uint32_t utcTime = gps_time / 1000000ULL;
const AP_Baro &baro = AP::baro();
int32_t altPres = INT_MAX;
if (baro.healthy()) {
// Altitude difference between sea level pressure and current pressure. Result in millimeters
altPres = baro.get_altitude_difference(SSL_AIR_PRESSURE, baro.get_pressure()) * 1E3; // convert m to mm;
}
mavlink_msg_uavionix_adsb_out_dynamic_send(
chan,
utcTime,
latitude,
longitude,
altGNSS,
fixType,
numSats,
altPres,
accHoriz,
accVert,
accVel,
velVert,
nsVog,
ewVog,
emStatus,
state,
squawk);
}
void AP_ADSB::send_dynamic_out(const mavlink_channel_t chan)
{
// --------------
// Knowns
AP_GPS gps = _ahrs.get_gps();
Vector3f gps_velocity = gps.velocity();
int32_t latitude = _my_loc.lat;
int32_t longitude = _my_loc.lng;
int32_t altGNSS = _my_loc.alt*0.1f; // convert cm to mm
int16_t velVert = gps_velocity.z * 1E2; // convert m/s to cm/s
int16_t nsVog = gps_velocity.x * 1E2; // convert m/s to cm/s
int16_t ewVog = gps_velocity.y * 1E2; // convert m/s to cm/s
uint8_t fixType = gps.status(); // this lines up perfectly with our enum
uint8_t emStatus = 0; // TODO: implement this ENUM. no emergency = 0
uint8_t numSats = gps.num_sats();
uint16_t squawk = 1200; // Mode A code (typically 1200 [0x04B0] for VFR)
uint32_t accHoriz = UINT_MAX;
float accHoriz_f;
if (gps.horizontal_accuracy(accHoriz_f)) {
accHoriz = accHoriz_f * 1E3; // convert m to mm
}
uint16_t accVert = USHRT_MAX;
float accVert_f;
if (gps.vertical_accuracy(accVert_f)) {
accVert = accVert_f * 1E2; // convert m to cm
}
uint16_t accVel = USHRT_MAX;
float accVel_f;
if (gps.speed_accuracy(accVel_f)) {
accVel = accVel_f * 1E3; // convert m/s to mm/s
}
uint16_t state = 0;
if (out_state._is_in_auto_mode) {
state |= UAVIONIX_ADSB_OUT_DYNAMIC_STATE_AUTOPILOT_ENABLED;
}
if (!out_state.is_flying) {
state |= UAVIONIX_ADSB_OUT_DYNAMIC_STATE_ON_GROUND;
}
// --------------
// Not Sure
uint32_t utcTime = UINT_MAX; // uint32_t utcTime,
// TODO: confirm this sets utcTime correctly
const uint64_t gps_time = gps.time_epoch_usec();
utcTime = gps_time / 1000000ULL;
// --------------
// Unknowns
// TODO: implement http://www.srh.noaa.gov/images/epz/wxcalc/pressureAltitude.pdf
int32_t altPres = INT_MAX; //_ahrs.get_baro().get_altitude() relative to home, not MSL
mavlink_msg_uavionix_adsb_out_dynamic_send(
chan,
utcTime,
latitude,
longitude,
altGNSS,
fixType,
numSats,
altPres,
accHoriz,
accVert,
accVel,
velVert,
nsVog,
ewVog,
emStatus,
state,
squawk);
}
