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synced 2024-11-29 07:24:13 +01:00
Added groundtruth simulation support.
This new UAVO serves principally to log data for future comparison with onboard estimation techniques. Conflicts: ground/openpilotgcs/src/plugins/hitl/il2simulator.cpp ground/openpilotgcs/src/plugins/hitl/simulator.h
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@ -202,6 +202,7 @@ void AeroSimRCSimulator::processUpdate(const QByteArray &data)
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/**********************************************************************************************/
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out.altitude = posZ;
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out.agl = posZ;
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out.heading = yaw * RAD2DEG;
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out.latitude = lat * 10e6;
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out.longitude = lon * 10e6;
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@ -268,9 +268,9 @@ void FGSimulator::processUpdate(const QByteArray& inp)
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// Get heading (deg)
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float heading = fields[14].toFloat();
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// Get altitude (m)
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float altitude = fields[15].toFloat() * FT2M;
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float altitude_msl = fields[15].toFloat() * FT2M;
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// Get altitudeAGL (m)
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float altitudeAGL = fields[16].toFloat() * FT2M;
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float altitude_agl = fields[16].toFloat() * FT2M;
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// Get groundspeed (m/s)
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float groundspeed = fields[17].toFloat() * KT2MPS;
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// Get airspeed (m/s)
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@ -299,7 +299,7 @@ void FGSimulator::processUpdate(const QByteArray& inp)
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float NED[3];
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// convert from cm back to meters
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double LLA[3] = {latitude, longitude, altitude};
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double LLA[3] = {latitude, longitude, altitude_msl};
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double ECEF[3];
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double RNE[9];
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Utils::CoordinateConversions().RneFromLLA(LLA,(double (*)[3])RNE);
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@ -310,7 +310,8 @@ void FGSimulator::processUpdate(const QByteArray& inp)
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// Update GPS Position objects
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out.latitude = latitude * 1e7;
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out.longitude = longitude * 1e7;
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out.altitude = altitude;
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out.altitude = altitude_msl;
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out.agl = altitude_agl;
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out.groundspeed = groundspeed;
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out.calibratedAirspeed = airspeed;
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@ -277,8 +277,9 @@ void IL2Simulator::processUpdate(const QByteArray& inp)
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// Update BaroAltitude object
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out.altitude = current.Z;
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out.temperature = TEMP_GROUND + (current.Z * TEMP_LAPSE_RATE) - 273.0;
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out.pressure = PRESSURE(current.Z)/1000.0; // kpa
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out.agl = current.Z;
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out.temperature = airParameters.groundTemp + (current.Z * airParameters.tempLapseRate) - 273.0;
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out.pressure = airPressureFromAltitude(current.Z, airParameters, gravity) ; // kpa
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// Update attActual object
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@ -138,7 +138,7 @@ void Simulator::onStart()
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actDesired = ActuatorDesired::GetInstance(objManager);
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actCommand = ActuatorCommand::GetInstance(objManager);
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manCtrlCommand = ManualControlCommand::GetInstance(objManager);
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gcsReceiver= GCSReceiver::GetInstance(objManager);
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gcsReceiver = GCSReceiver::GetInstance(objManager);
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flightStatus = FlightStatus::GetInstance(objManager);
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posHome = HomeLocation::GetInstance(objManager);
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velActual = VelocityActual::GetInstance(objManager);
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@ -152,6 +152,7 @@ void Simulator::onStart()
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gpsPos = GPSPosition::GetInstance(objManager);
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gpsVel = GPSVelocity::GetInstance(objManager);
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telStats = GCSTelemetryStats::GetInstance(objManager);
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groundTruth = GroundTruth::GetInstance(objManager);
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// Listen to autopilot connection events
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TelemetryManager* telMngr = pm->getObject<TelemetryManager>();
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@ -392,6 +393,7 @@ void Simulator::updateUAVOs(Output2Hardware out){
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memset(&noise, 0, sizeof(Noise));
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}
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/*******************************/
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HomeLocation::DataFields homeData = posHome->getData();
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if(!once)
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{
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@ -401,7 +403,7 @@ void Simulator::updateUAVOs(Output2Hardware out){
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// Update homelocation
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homeData.Latitude = out.latitude; //Already in *10^7 integer format
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homeData.Longitude = out.longitude; //Already in *10^7 integer format
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homeData.Altitude = out.altitude;
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homeData.Altitude = out.agl;
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double LLA[3];
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LLA[0]=out.latitude;
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LLA[1]=out.longitude;
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@ -424,7 +426,36 @@ void Simulator::updateUAVOs(Output2Hardware out){
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once=true;
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}
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/*******************************/
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//Copy everything to the ground truth object. GroundTruth is Noise-free.
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GroundTruth::DataFields groundTruthData;
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groundTruthData = groundTruth->getData();
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groundTruthData.AngularRates[0]=out.rollRate;
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groundTruthData.AngularRates[1]=out.pitchRate;
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groundTruthData.AngularRates[2]=out.yawRate;
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groundTruthData.CalibratedAirspeed=out.calibratedAirspeed;
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groundTruthData.TrueAirspeed=out.trueAirspeed;
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groundTruthData.AngleOfAttack=out.angleOfAttack;
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groundTruthData.AngleOfSlip=out.angleOfSlip;
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groundTruthData.PositionNED[0]=out.dstN-initN;
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groundTruthData.PositionNED[1]=out.dstE-initD;
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groundTruthData.PositionNED[2]=out.dstD-initD;
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groundTruthData.VelocityNED[0]=out.velNorth;
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groundTruthData.VelocityNED[1]=out.velEast;
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groundTruthData.VelocityNED[2]=out.velDown;
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groundTruthData.RPY[0]=out.roll;
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groundTruthData.RPY[0]=out.pitch;
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groundTruthData.RPY[0]=out.heading;
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//Set UAVO
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groundTruth->setData(groundTruthData);
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/*******************************/
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// Update attActual object
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AttitudeActual::DataFields attActualData;
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attActualData = attActual->getData();
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@ -574,6 +605,7 @@ void Simulator::updateUAVOs(Output2Hardware out){
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/*****************************************/
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}
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/*******************************/
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if (settings.gcsReceiverEnabled) {
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if (gcsRcvrTime.msecsTo(currentTime) >= settings.minOutputPeriod) {
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GCSReceiver::DataFields gcsRcvrData;
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@ -591,6 +623,7 @@ void Simulator::updateUAVOs(Output2Hardware out){
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}
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/*******************************/
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if (settings.gpsPositionEnabled) {
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if (gpsPosTime.msecsTo(currentTime) >= settings.gpsPosRate) {
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qDebug()<< " GPS time:" << gpsPosTime << ", currentTime: " << currentTime << ", difference: " << gpsPosTime.msecsTo(currentTime);
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@ -623,6 +656,7 @@ void Simulator::updateUAVOs(Output2Hardware out){
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}
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}
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/*******************************/
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// Update VelocityActual.{North,East,Down}
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if (settings.groundTruthEnabled) {
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if (groundTruthTime.msecsTo(currentTime) >= settings.groundTruthRate) {
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@ -645,6 +679,7 @@ void Simulator::updateUAVOs(Output2Hardware out){
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}
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}
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// /*******************************/
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// if (settings.sonarAltitude) {
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// static QTime sonarAltTime = currentTime;
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// if (sonarAltTime.msecsTo(currentTime) >= settings.sonarAltRate) {
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@ -666,6 +701,7 @@ void Simulator::updateUAVOs(Output2Hardware out){
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// }
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// }
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/*******************************/
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// Update BaroAltitude object
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if (settings.baroAltitudeEnabled){
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if (baroAltTime.msecsTo(currentTime) >= settings.baroAltRate) {
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@ -680,6 +716,7 @@ void Simulator::updateUAVOs(Output2Hardware out){
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}
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}
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/*******************************/
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// Update AirspeedActual object
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if (settings.airspeedActualEnabled){
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if (airspeedActualTime.msecsTo(currentTime) >= settings.airspeedActualRate) {
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@ -692,6 +729,7 @@ void Simulator::updateUAVOs(Output2Hardware out){
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}
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}
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/*******************************/
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// Update raw attitude sensors
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if (settings.attRawEnabled) {
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if (attRawTime.msecsTo(currentTime) >= settings.attRawRate) {
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@ -50,6 +50,7 @@
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#include "gcstelemetrystats.h"
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#include "gpsposition.h"
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#include "gpsvelocity.h"
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#include "groundtruth.h"
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#include "gyros.h"
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#include "homelocation.h"
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#include "manualcontrolcommand.h"
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@ -150,9 +151,13 @@ struct Output2Hardware{
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float latitude;
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float longitude;
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float altitude;
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float agl; //[m]
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float heading;
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float groundspeed; //[m/s]
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float calibratedAirspeed; //[m/s]
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float groundspeed; //[m/s]
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float calibratedAirspeed; //[m/s]
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float trueAirspeed; //[m/s]
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float angleOfAttack;
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float angleOfSlip;
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float roll;
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float pitch;
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float pressure;
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@ -166,10 +171,10 @@ struct Output2Hardware{
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float accX; //[m/s^2]
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float accY; //[m/s^2]
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float accZ; //[m/s^2]
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float rollRate; //[deg/s]
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float pitchRate; //[deg/s]
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float yawRate; //[deg/s]
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float delT;
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float rollRate; //[deg/s]
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float pitchRate; //[deg/s]
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float yawRate; //[deg/s]
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float delT; //[s]
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float rc_channel[GCSReceiver::CHANNEL_NUMELEM]; //Elements in rc_channel are between -1 and 1
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@ -275,6 +280,7 @@ protected:
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Gyros* gyros;
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GCSTelemetryStats* telStats;
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GCSReceiver* gcsReceiver;
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GroundTruth* groundTruth;
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SimulatorSettings settings;
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@ -195,7 +195,8 @@ void XplaneSimulator::transmitUpdate()
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*/
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void XplaneSimulator::processUpdate(const QByteArray& dataBuf)
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{
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float altitude = 0;
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float altitude_msl = 0;
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float altitude_agl = 0;
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float latitude = 0;
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float longitude = 0;
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float airspeed_keas = 0;
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@ -239,7 +240,8 @@ void XplaneSimulator::processUpdate(const QByteArray& dataBuf)
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case XplaneSimulator::LatitudeLongitudeAltitude:
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latitude = *((float*)(buf.data()+4*1));
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longitude = *((float*)(buf.data()+4*2));
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altitude = *((float*)(buf.data()+4*3))* FT2M;
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altitude_msl = *((float*)(buf.data()+4*3))* FT2M;
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altitude_agl = *((float*)(buf.data()+4*4))* FT2M;
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break;
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case XplaneSimulator::Speed:
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@ -302,7 +304,8 @@ void XplaneSimulator::processUpdate(const QByteArray& dataBuf)
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// Update GPS Position objects
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out.latitude = latitude * 1e7;
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out.longitude = longitude * 1e7;
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out.altitude = altitude;
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out.altitude = altitude_msl;
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out.agl = altitude_agl;
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out.groundspeed = groundspeed_ktgs*1.15*1.6089/3.6; //Convert from [kts] to [m/s]
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out.calibratedAirspeed = airspeed_keas*1.15*1.6089/3.6; //Convert from [kts] to [m/s]
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@ -61,6 +61,7 @@ HEADERS += $$UAVOBJECT_SYNTHETICS/accessorydesired.h \
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$$UAVOBJECT_SYNTHETICS/mixerstatus.h \
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$$UAVOBJECT_SYNTHETICS/velocitydesired.h \
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$$UAVOBJECT_SYNTHETICS/velocityactual.h \
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$$UAVOBJECT_SYNTHETICS/groundtruth.h \
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$$UAVOBJECT_SYNTHETICS/guidancesettings.h \
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$$UAVOBJECT_SYNTHETICS/positiondesired.h \
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$$UAVOBJECT_SYNTHETICS/relaytuning.h \
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@ -128,6 +129,7 @@ SOURCES += $$UAVOBJECT_SYNTHETICS/accessorydesired.cpp \
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$$UAVOBJECT_SYNTHETICS/mixerstatus.cpp \
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$$UAVOBJECT_SYNTHETICS/velocitydesired.cpp \
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$$UAVOBJECT_SYNTHETICS/velocityactual.cpp \
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$$UAVOBJECT_SYNTHETICS/groundtruth.cpp \
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$$UAVOBJECT_SYNTHETICS/guidancesettings.cpp \
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$$UAVOBJECT_SYNTHETICS/positiondesired.cpp \
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$$UAVOBJECT_SYNTHETICS/relaytuningsettings.cpp \
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17
shared/uavobjectdefinition/groundtruth.xml
Normal file
17
shared/uavobjectdefinition/groundtruth.xml
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<xml>
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<object name="GroundTruth" singleinstance="true" settings="false">
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<description>The updated Attitude estimation from @ref AHRSCommsModule.</description>
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<field name="PositionNED" units="m" type="float" elements="3"/>
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<field name="VelocityNED" units="m" type="float" elements="3"/>
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<field name="RPY" units="deg" type="float" elements="3"/>
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<field name="AngularRates" units="deg/s" type="float" elements="3"/>
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<field name="TrueAirspeed" units="m/s" type="float" elements="1"/>
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<field name="CalibratedAirspeed" units="m/s" type="float" elements="1"/>
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<field name="AngleOfAttack" units="deg" type="float" elements="1"/>
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<field name="AngleOfSlip" units="deg" type="float" elements="1"/>
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<access gcs="readwrite" flight="readonly"/>
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<telemetrygcs acked="false" updatemode="periodic" period="50"/>
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<telemetryflight acked="false" updatemode="manual" period="50000"/>
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<logging updatemode="manual" period="0"/>
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</object>
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</xml>
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