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https://github.com/ArduPilot/ardupilot
synced 2025-01-22 00:28:30 -04:00
AP_NavEKF3: use GPS singleton
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9c8466dc03
commit
5dc714bf5f
@ -629,7 +629,7 @@ void NavEKF3::check_log_write(void)
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logging.log_compass = false;
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}
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if (logging.log_gps) {
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DataFlash_Class::instance()->Log_Write_GPS(_ahrs->get_gps(), _ahrs->get_gps().primary_sensor(), imuSampleTime_us);
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DataFlash_Class::instance()->Log_Write_GPS(AP::gps(), AP::gps().primary_sensor(), imuSampleTime_us);
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logging.log_gps = false;
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}
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if (logging.log_baro) {
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@ -479,7 +479,7 @@ bool NavEKF3_core::setOriginLLH(const Location &loc)
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void NavEKF3_core::setOrigin()
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{
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// assume origin at current GPS location (no averaging)
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EKF_origin = _ahrs->get_gps().location();
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EKF_origin = AP::gps().location();
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// if flying, correct for height change from takeoff so that the origin is at field elevation
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if (inFlight) {
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EKF_origin.alt += (int32_t)(100.0f * stateStruct.position.z);
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@ -456,8 +456,10 @@ void NavEKF3_core::readGpsData()
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{
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// check for new GPS data
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// limit update rate to avoid overflowing the FIFO buffer
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if (_ahrs->get_gps().last_message_time_ms() - lastTimeGpsReceived_ms > frontend->sensorIntervalMin_ms) {
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if (_ahrs->get_gps().status() >= AP_GPS::GPS_OK_FIX_3D) {
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const AP_GPS &gps = AP::gps();
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if (gps.last_message_time_ms() - lastTimeGpsReceived_ms > frontend->sensorIntervalMin_ms) {
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if (gps.status() >= AP_GPS::GPS_OK_FIX_3D) {
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// report GPS fix status
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gpsCheckStatus.bad_fix = false;
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@ -465,13 +467,13 @@ void NavEKF3_core::readGpsData()
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secondLastGpsTime_ms = lastTimeGpsReceived_ms;
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// get current fix time
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lastTimeGpsReceived_ms = _ahrs->get_gps().last_message_time_ms();
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lastTimeGpsReceived_ms = gps.last_message_time_ms();
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// estimate when the GPS fix was valid, allowing for GPS processing and other delays
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// ideally we should be using a timing signal from the GPS receiver to set this time
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// Use the driver specified delay
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float gps_delay_sec = 0;
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_ahrs->get_gps().get_lag(gps_delay_sec);
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gps.get_lag(gps_delay_sec);
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gpsDataNew.time_ms = lastTimeGpsReceived_ms - (uint32_t)(gps_delay_sec * 1000.0f);
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// Correct for the average intersampling delay due to the filter updaterate
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@ -481,17 +483,17 @@ void NavEKF3_core::readGpsData()
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gpsDataNew.time_ms = MIN(MAX(gpsDataNew.time_ms,imuDataDelayed.time_ms),imuDataDownSampledNew.time_ms);
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// Get which GPS we are using for position information
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gpsDataNew.sensor_idx = _ahrs->get_gps().primary_sensor();
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gpsDataNew.sensor_idx = gps.primary_sensor();
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// read the NED velocity from the GPS
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gpsDataNew.vel = _ahrs->get_gps().velocity();
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gpsDataNew.vel = gps.velocity();
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// Use the speed and position accuracy from the GPS if available, otherwise set it to zero.
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// Apply a decaying envelope filter with a 5 second time constant to the raw accuracy data
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float alpha = constrain_float(0.0002f * (lastTimeGpsReceived_ms - secondLastGpsTime_ms),0.0f,1.0f);
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gpsSpdAccuracy *= (1.0f - alpha);
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float gpsSpdAccRaw;
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if (!_ahrs->get_gps().speed_accuracy(gpsSpdAccRaw)) {
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if (!gps.speed_accuracy(gpsSpdAccRaw)) {
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gpsSpdAccuracy = 0.0f;
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} else {
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gpsSpdAccuracy = MAX(gpsSpdAccuracy,gpsSpdAccRaw);
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@ -499,7 +501,7 @@ void NavEKF3_core::readGpsData()
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}
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gpsPosAccuracy *= (1.0f - alpha);
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float gpsPosAccRaw;
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if (!_ahrs->get_gps().horizontal_accuracy(gpsPosAccRaw)) {
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if (!gps.horizontal_accuracy(gpsPosAccRaw)) {
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gpsPosAccuracy = 0.0f;
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} else {
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gpsPosAccuracy = MAX(gpsPosAccuracy,gpsPosAccRaw);
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@ -507,7 +509,7 @@ void NavEKF3_core::readGpsData()
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}
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gpsHgtAccuracy *= (1.0f - alpha);
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float gpsHgtAccRaw;
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if (!_ahrs->get_gps().vertical_accuracy(gpsHgtAccRaw)) {
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if (!gps.vertical_accuracy(gpsHgtAccRaw)) {
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gpsHgtAccuracy = 0.0f;
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} else {
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gpsHgtAccuracy = MAX(gpsHgtAccuracy,gpsHgtAccRaw);
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@ -515,16 +517,16 @@ void NavEKF3_core::readGpsData()
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}
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// check if we have enough GPS satellites and increase the gps noise scaler if we don't
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if (_ahrs->get_gps().num_sats() >= 6 && (PV_AidingMode == AID_ABSOLUTE)) {
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if (gps.num_sats() >= 6 && (PV_AidingMode == AID_ABSOLUTE)) {
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gpsNoiseScaler = 1.0f;
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} else if (_ahrs->get_gps().num_sats() == 5 && (PV_AidingMode == AID_ABSOLUTE)) {
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} else if (gps.num_sats() == 5 && (PV_AidingMode == AID_ABSOLUTE)) {
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gpsNoiseScaler = 1.4f;
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} else { // <= 4 satellites or in constant position mode
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gpsNoiseScaler = 2.0f;
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}
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// Check if GPS can output vertical velocity, vertical velocity use is permitted and set GPS fusion mode accordingly
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if (_ahrs->get_gps().have_vertical_velocity() && (frontend->_fusionModeGPS == 0) && !frontend->inhibitGpsVertVelUse) {
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if (gps.have_vertical_velocity() && (frontend->_fusionModeGPS == 0) && !frontend->inhibitGpsVertVelUse) {
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useGpsVertVel = true;
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} else {
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useGpsVertVel = false;
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@ -542,7 +544,7 @@ void NavEKF3_core::readGpsData()
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calcGpsGoodForFlight();
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// Read the GPS location in WGS-84 lat,long,height coordinates
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const struct Location &gpsloc = _ahrs->get_gps().location();
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const struct Location &gpsloc = gps.location();
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// Set the EKF origin and magnetic field declination if not previously set and GPS checks have passed
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if (gpsGoodToAlign && !validOrigin) {
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@ -249,9 +249,9 @@ bool NavEKF3_core::getPosNE(Vector2f &posNE) const
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} else {
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// In constant position mode the EKF position states are at the origin, so we cannot use them as a position estimate
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if(validOrigin) {
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if ((_ahrs->get_gps().status() >= AP_GPS::GPS_OK_FIX_2D)) {
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if ((AP::gps().status() >= AP_GPS::GPS_OK_FIX_2D)) {
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// If the origin has been set and we have GPS, then return the GPS position relative to the origin
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const struct Location &gpsloc = _ahrs->get_gps().location();
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const struct Location &gpsloc = AP::gps().location();
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Vector2f tempPosNE = location_diff(EKF_origin, gpsloc);
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posNE.x = tempPosNE.x;
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posNE.y = tempPosNE.y;
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@ -312,6 +312,8 @@ bool NavEKF3_core::getHAGL(float &HAGL) const
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// The getFilterStatus() function provides a more detailed description of data health and must be checked if data is to be used for flight control
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bool NavEKF3_core::getLLH(struct Location &loc) const
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{
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const AP_GPS &gps = AP::gps();
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if(validOrigin) {
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// Altitude returned is an absolute altitude relative to the WGS-84 spherioid
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loc.alt = 100 * (int32_t)(ekfGpsRefHgt - (double)outputDataNew.position.z);
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@ -327,9 +329,9 @@ bool NavEKF3_core::getLLH(struct Location &loc) const
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} else {
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// we could be in constant position mode because the vehicle has taken off without GPS, or has lost GPS
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// in this mode we cannot use the EKF states to estimate position so will return the best available data
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if ((_ahrs->get_gps().status() >= AP_GPS::GPS_OK_FIX_2D)) {
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if ((gps.status() >= AP_GPS::GPS_OK_FIX_2D)) {
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// we have a GPS position fix to return
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const struct Location &gpsloc = _ahrs->get_gps().location();
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const struct Location &gpsloc = gps.location();
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loc.lat = gpsloc.lat;
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loc.lng = gpsloc.lng;
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return true;
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@ -342,8 +344,8 @@ bool NavEKF3_core::getLLH(struct Location &loc) const
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} else {
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// If no origin has been defined for the EKF, then we cannot use its position states so return a raw
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// GPS reading if available and return false
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if ((_ahrs->get_gps().status() >= AP_GPS::GPS_OK_FIX_3D)) {
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const struct Location &gpsloc = _ahrs->get_gps().location();
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if ((gps.status() >= AP_GPS::GPS_OK_FIX_3D)) {
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const struct Location &gpsloc = gps.location();
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loc = gpsloc;
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loc.flags.relative_alt = 0;
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loc.flags.terrain_alt = 0;
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@ -242,7 +242,7 @@ void NavEKF3_core::SelectVelPosFusion()
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// Determine if we need to fuse position and velocity data on this time step
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if (gpsDataToFuse && PV_AidingMode == AID_ABSOLUTE) {
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// correct GPS data for position offset of antenna phase centre relative to the IMU
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Vector3f posOffsetBody = _ahrs->get_gps().get_antenna_offset(gpsDataDelayed.sensor_idx) - accelPosOffset;
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Vector3f posOffsetBody = AP::gps().get_antenna_offset(gpsDataDelayed.sensor_idx) - accelPosOffset;
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if (!posOffsetBody.is_zero()) {
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if (fuseVelData) {
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// TODO use a filtered angular rate with a group delay that matches the GPS delay
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@ -43,7 +43,9 @@ bool NavEKF3_core::calcGpsGoodToAlign(void)
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// Check for significant change in GPS position if disarmed which indicates bad GPS
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// This check can only be used when the vehicle is stationary
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const struct Location &gpsloc = _ahrs->get_gps().location(); // Current location
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const AP_GPS &gps = AP::gps();
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const struct Location &gpsloc = gps.location(); // Current location
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const float posFiltTimeConst = 10.0f; // time constant used to decay position drift
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// calculate time lapsesd since last update and limit to prevent numerical errors
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float deltaTime = constrain_float(float(imuDataDelayed.time_ms - lastPreAlignGpsCheckTime_ms)*0.001f,0.01f,posFiltTimeConst);
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@ -71,18 +73,18 @@ bool NavEKF3_core::calcGpsGoodToAlign(void)
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// Check that the vertical GPS vertical velocity is reasonable after noise filtering
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bool gpsVertVelFail;
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if (_ahrs->get_gps().have_vertical_velocity() && onGround) {
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if (gps.have_vertical_velocity() && onGround) {
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// check that the average vertical GPS velocity is close to zero
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gpsVertVelFilt = 0.1f * gpsDataNew.vel.z + 0.9f * gpsVertVelFilt;
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gpsVertVelFilt = constrain_float(gpsVertVelFilt,-10.0f,10.0f);
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gpsVertVelFail = (fabsf(gpsVertVelFilt) > 0.3f*checkScaler) && (frontend->_gpsCheck & MASK_GPS_VERT_SPD);
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} else if ((frontend->_fusionModeGPS == 0) && !_ahrs->get_gps().have_vertical_velocity()) {
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} else if ((frontend->_fusionModeGPS == 0) && !gps.have_vertical_velocity()) {
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// If the EKF settings require vertical GPS velocity and the receiver is not outputting it, then fail
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gpsVertVelFail = true;
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// if we have a 3D fix with no vertical velocity and
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// EK3_GPS_TYPE=0 then change it to 1. It means the GPS is not
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// capable of giving a vertical velocity
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if (_ahrs->get_gps().status() >= AP_GPS::GPS_OK_FIX_3D) {
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if (gps.status() >= AP_GPS::GPS_OK_FIX_3D) {
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frontend->_fusionModeGPS.set(1);
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gcs().send_text(MAV_SEVERITY_WARNING, "EK3: Changed EK3_GPS_TYPE to 1");
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}
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@ -124,7 +126,7 @@ bool NavEKF3_core::calcGpsGoodToAlign(void)
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// fail if horiziontal position accuracy not sufficient
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float hAcc = 0.0f;
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bool hAccFail;
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if (_ahrs->get_gps().horizontal_accuracy(hAcc)) {
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if (gps.horizontal_accuracy(hAcc)) {
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hAccFail = (hAcc > 5.0f*checkScaler) && (frontend->_gpsCheck & MASK_GPS_POS_ERR);
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} else {
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hAccFail = false;
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@ -144,7 +146,7 @@ bool NavEKF3_core::calcGpsGoodToAlign(void)
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// Check for vertical GPS accuracy
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float vAcc = 0.0f;
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bool vAccFail = false;
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if (_ahrs->get_gps().vertical_accuracy(vAcc)) {
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if (gps.vertical_accuracy(vAcc)) {
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vAccFail = (vAcc > 7.5f * checkScaler) && (frontend->_gpsCheck & MASK_GPS_POS_ERR);
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}
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// Report check result as a text string and bitmask
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@ -171,24 +173,24 @@ bool NavEKF3_core::calcGpsGoodToAlign(void)
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}
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// fail if satellite geometry is poor
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bool hdopFail = (_ahrs->get_gps().get_hdop() > 250) && (frontend->_gpsCheck & MASK_GPS_HDOP);
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bool hdopFail = (gps.get_hdop() > 250) && (frontend->_gpsCheck & MASK_GPS_HDOP);
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// Report check result as a text string and bitmask
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if (hdopFail) {
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hal.util->snprintf(prearm_fail_string, sizeof(prearm_fail_string),
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"GPS HDOP %.1f (needs 2.5)", (double)(0.01f * _ahrs->get_gps().get_hdop()));
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"GPS HDOP %.1f (needs 2.5)", (double)(0.01f * gps.get_hdop()));
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gpsCheckStatus.bad_hdop = true;
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} else {
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gpsCheckStatus.bad_hdop = false;
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}
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// fail if not enough sats
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bool numSatsFail = (_ahrs->get_gps().num_sats() < 6) && (frontend->_gpsCheck & MASK_GPS_NSATS);
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bool numSatsFail = (gps.num_sats() < 6) && (frontend->_gpsCheck & MASK_GPS_NSATS);
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// Report check result as a text string and bitmask
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if (numSatsFail) {
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hal.util->snprintf(prearm_fail_string, sizeof(prearm_fail_string),
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"GPS numsats %u (needs 6)", _ahrs->get_gps().num_sats());
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"GPS numsats %u (needs 6)", gps.num_sats());
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gpsCheckStatus.bad_sats = true;
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} else {
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gpsCheckStatus.bad_sats = false;
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@ -250,7 +252,7 @@ void NavEKF3_core::calcGpsGoodForFlight(void)
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// get the receivers reported speed accuracy
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float gpsSpdAccRaw;
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if (!_ahrs->get_gps().speed_accuracy(gpsSpdAccRaw)) {
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if (!AP::gps().speed_accuracy(gpsSpdAccRaw)) {
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gpsSpdAccRaw = 0.0f;
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}
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@ -72,7 +72,7 @@ bool NavEKF3_core::setup_core(NavEKF3 *_frontend, uint8_t _imu_index, uint8_t _c
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if (_frontend->_fusionModeGPS != 3) {
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// Wait for the configuration of all GPS units to be confirmed. Until this has occurred the GPS driver cannot provide a correct time delay
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float gps_delay_sec = 0;
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if (!_ahrs->get_gps().get_lag(gps_delay_sec)) {
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if (!AP::gps().get_lag(gps_delay_sec)) {
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if (AP_HAL::millis() - lastInitFailReport_ms > 10000) {
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lastInitFailReport_ms = AP_HAL::millis();
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// provide an escalating series of messages
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@ -397,7 +397,7 @@ void NavEKF3_core::InitialiseVariables()
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bool NavEKF3_core::InitialiseFilterBootstrap(void)
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{
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// If we are a plane and don't have GPS lock then don't initialise
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if (assume_zero_sideslip() && _ahrs->get_gps().status() < AP_GPS::GPS_OK_FIX_3D) {
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if (assume_zero_sideslip() && AP::gps().status() < AP_GPS::GPS_OK_FIX_3D) {
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statesInitialised = false;
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return false;
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}
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