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Extended HiTL API to the rest of the simulators.
This commit is contained in:
parent
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commit
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@ -34,9 +34,6 @@
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#define M_PI 3.14159265358979323846
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#define M_PI 3.14159265358979323846
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#endif
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#endif
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//FGSimulator::FGSimulator(QString hostAddr, int outPort, int inPort, bool manual, QString binPath, QString dataPath) :
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//FGSimulator::FGSimulator(QString hostAddr, int outPort, int inPort, bool manual, QString binPath, QString dataPath) :
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// Simulator(hostAddr, outPort, inPort, manual, binPath, dataPath),
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// Simulator(hostAddr, outPort, inPort, manual, binPath, dataPath),
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// fgProcess(NULL)
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// fgProcess(NULL)
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@ -63,8 +60,6 @@ FGSimulator::~FGSimulator()
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void FGSimulator::setupUdpPorts(const QString& host, int inPort, int outPort)
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void FGSimulator::setupUdpPorts(const QString& host, int inPort, int outPort)
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{
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{
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Q_UNUSED(outPort);
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if(inSocket->bind(QHostAddress(host), inPort))
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if(inSocket->bind(QHostAddress(host), inPort))
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emit processOutput("Successfully bound to address " + host + " on port " + QString::number(inPort) + "\n");
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emit processOutput("Successfully bound to address " + host + " on port " + QString::number(inPort) + "\n");
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else
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else
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@ -78,14 +73,14 @@ bool FGSimulator::setupProcess()
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// Copy FlightGear generic protocol configuration file to the FG protocol directory
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// Copy FlightGear generic protocol configuration file to the FG protocol directory
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// NOTE: Not working on Windows 7, if FG is installed in the "Program Files",
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// NOTE: Not working on Windows 7, if FG is installed in the "Program Files",
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// likelly due to permissions. The file should be manually copied to data/Protocol/opfgprotocol.xml
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// likelly due to permissions. The file should be manually copied to data/Protocol/opfgprotocol.xml
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// QFile xmlFile(":/flightgear/genericprotocol/opfgprotocol.xml");
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// QFile xmlFile(":/flightgear/genericprotocol/opfgprotocol.xml");
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// xmlFile.open(QIODevice::ReadOnly | QIODevice::Text);
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// xmlFile.open(QIODevice::ReadOnly | QIODevice::Text);
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// QString xml = xmlFile.readAll();
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// QString xml = xmlFile.readAll();
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// xmlFile.close();
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// xmlFile.close();
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// QFile xmlFileOut(pathData + "/Protocol/opfgprotocol.xml");
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// QFile xmlFileOut(pathData + "/Protocol/opfgprotocol.xml");
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// xmlFileOut.open(QIODevice::WriteOnly | QIODevice::Text);
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// xmlFileOut.open(QIODevice::WriteOnly | QIODevice::Text);
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// xmlFileOut.write(xml.toAscii());
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// xmlFileOut.write(xml.toAscii());
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// xmlFileOut.close();
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// xmlFileOut.close();
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Qt::HANDLE mainThread = QThread::currentThreadId();
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Qt::HANDLE mainThread = QThread::currentThreadId();
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qDebug() << "setupProcess Thread: "<< mainThread;
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qDebug() << "setupProcess Thread: "<< mainThread;
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@ -237,22 +232,21 @@ void FGSimulator::transmitUpdate()
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void FGSimulator::processUpdate(const QByteArray& inp)
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void FGSimulator::processUpdate(const QByteArray& inp)
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{
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{
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//TODO: this does not use the FLIGHT_PARAM structure, it should!
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//TODO: this does not use the FLIGHT_PARAM structure, it should!
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static char once=0;
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// Split
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// Split
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QString data(inp);
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QString data(inp);
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QStringList fields = data.split(",");
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QStringList fields = data.split(",");
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// Get xRate (deg/s)
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// Get xRate (deg/s)
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// float xRate = fields[0].toFloat() * 180.0/M_PI;
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// float xRate = fields[0].toFloat() * 180.0/M_PI;
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// Get yRate (deg/s)
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// Get yRate (deg/s)
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// float yRate = fields[1].toFloat() * 180.0/M_PI;
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// float yRate = fields[1].toFloat() * 180.0/M_PI;
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// Get zRate (deg/s)
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// Get zRate (deg/s)
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// float zRate = fields[2].toFloat() * 180.0/M_PI;
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// float zRate = fields[2].toFloat() * 180.0/M_PI;
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// Get xAccel (m/s^2)
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// Get xAccel (m/s^2)
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// float xAccel = fields[3].toFloat() * FT2M;
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float xAccel = fields[3].toFloat() * FT2M;
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// Get yAccel (m/s^2)
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// Get yAccel (m/s^2)
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// float yAccel = fields[4].toFloat() * FT2M;
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float yAccel = fields[4].toFloat() * FT2M;
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// Get xAccel (m/s^2)
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// Get xAccel (m/s^2)
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// float zAccel = fields[5].toFloat() * FT2M;
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float zAccel = fields[5].toFloat() * FT2M;
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// Get pitch (deg)
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// Get pitch (deg)
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float pitch = fields[6].toFloat();
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float pitch = fields[6].toFloat();
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// Get pitchRate (deg/s)
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// Get pitchRate (deg/s)
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@ -278,7 +272,7 @@ void FGSimulator::processUpdate(const QByteArray& inp)
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// Get groundspeed (m/s)
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// Get groundspeed (m/s)
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float groundspeed = fields[17].toFloat() * KT2MPS;
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float groundspeed = fields[17].toFloat() * KT2MPS;
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// Get airspeed (m/s)
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// Get airspeed (m/s)
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// float airspeed = fields[18].toFloat() * KT2MPS;
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float airspeed = fields[18].toFloat() * KT2MPS;
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// Get temperature (degC)
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// Get temperature (degC)
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float temperature = fields[19].toFloat();
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float temperature = fields[19].toFloat();
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// Get pressure (kpa)
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// Get pressure (kpa)
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@ -294,112 +288,60 @@ void FGSimulator::processUpdate(const QByteArray& inp)
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int n = fields[24].toInt();
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int n = fields[24].toInt();
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udpCounterFGrecv = n;
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udpCounterFGrecv = n;
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//run once
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///////
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HomeLocation::DataFields homeData = posHome->getData();
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// Output formatting
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if(!once)
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///////
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{
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Output2OP out;
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memset(&homeData, 0, sizeof(HomeLocation::DataFields));
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memset(&out, 0, sizeof(Output2OP));
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// Update homelocation
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homeData.Latitude = latitude * 10e6;
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homeData.Longitude = longitude * 10e6;
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homeData.Altitude = 0;
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double LLA[3];
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LLA[0]=latitude;
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LLA[1]=longitude;
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LLA[2]=0;
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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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Utils::CoordinateConversions().LLA2ECEF(LLA,ECEF);
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homeData.Be[0]=0;
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homeData.Be[1]=0;
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homeData.Be[2]=0;
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posHome->setData(homeData);
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once=1;
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}
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// Update VelocityActual.{Nort,East,Down}
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VelocityActual::DataFields velocityActualData;
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memset(&velocityActualData, 0, sizeof(VelocityActual::DataFields));
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velocityActualData.North = velocityActualNorth;
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velocityActualData.East = velocityActualEast;
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velocityActualData.Down = velocityActualDown;
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velActual->setData(velocityActualData);
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// Update PositionActual.{Nort,East,Down}
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PositionActual::DataFields positionActualData;
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memset(&positionActualData, 0, sizeof(PositionActual::DataFields));
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positionActualData.North = 0; //Currently hardcoded as there is no way of setting up a reference point to calculate distance
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positionActualData.East = 0; //Currently hardcoded as there is no way of setting up a reference point to calculate distance
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positionActualData.Down = altitude ; //Multiply by 1 because positionActual expects input in meters.
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posActual->setData(positionActualData);
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// Update AltitudeActual object
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BaroAltitude::DataFields baroAltData;
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memset(&baroAltData, 0, sizeof(BaroAltitude::DataFields));
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baroAltData.Altitude = altitudeAGL;
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baroAltData.Temperature = temperature;
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baroAltData.Pressure = pressure;
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baroAlt->setData(baroAltData);
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// Update attActual object
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AttitudeActual::DataFields attActualData;
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memset(&attActualData, 0, sizeof(AttitudeActual::DataFields));
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attActualData.Roll = roll;
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attActualData.Pitch = pitch;
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attActualData.Yaw = yaw;
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attActualData.q1 = 0;
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attActualData.q2 = 0;
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attActualData.q3 = 0;
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attActualData.q4 = 0;
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attActual->setData(attActualData);
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// Update gps objects
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GPSPosition::DataFields gpsData;
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memset(&gpsData, 0, sizeof(GPSPosition::DataFields));
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gpsData.Altitude = altitude;
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gpsData.Heading = heading;
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gpsData.Groundspeed = groundspeed;
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gpsData.Latitude = latitude*1e7;
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gpsData.Longitude = longitude*1e7;
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gpsData.Satellites = 10;
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gpsData.Status = GPSPosition::STATUS_FIX3D;
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gpsPos->setData(gpsData);
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float NED[3];
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float NED[3];
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// convert from cm back to meters
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// convert from cm back to meters
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double hLLA[3] = {(double) homeData.Latitude / 1e7, (double) homeData.Longitude / 1e7, (double) (homeData.Altitude)};
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double LLA[3] = {latitude, longitude, altitude};
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double ECEF[3];
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double ECEF[3];
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double RNE[9];
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double RNE[9];
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Utils::CoordinateConversions().RneFromLLA(hLLA,(double (*)[3])RNE);
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Utils::CoordinateConversions().RneFromLLA(LLA,(double (*)[3])RNE);
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Utils::CoordinateConversions().LLA2ECEF(hLLA,ECEF);
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Utils::CoordinateConversions().LLA2ECEF(LLA,ECEF);
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Utils::CoordinateConversions().LLA2Base(hLLA, ECEF, (float (*)[3]) RNE, NED);
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Utils::CoordinateConversions().LLA2Base(LLA, ECEF, (float (*)[3]) RNE, NED);
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positionActualData.North = NED[0]; //Currently hardcoded as there is no way of setting up a reference point to calculate distance
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positionActualData.East = NED[1]; //Currently hardcoded as there is no way of setting up a reference point to calculate distance
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positionActualData.Down = NED[2]; //Multiply by 1 because positionActual expects input in meters.
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posActual->setData(positionActualData);
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// Update AttitudeRaw object (filtered gyros only for now)
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// Update GPS Position objects
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//AttitudeRaw::DataFields rawData;
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out.latitude = latitude * 1e7;
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//AttitudeRaw::DataFields rawData;
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out.longitude = longitude * 1e7;
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Gyros::DataFields gyroData;
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out.altitude = altitude;
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Accels::DataFields accelData;
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out.groundspeed = groundspeed;
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memset(&gyroData, 0, sizeof(Gyros::DataFields));
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memset(&accelData, 0, sizeof(Accels::DataFields));
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out.calibratedAirspeed = airspeed;
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gyroData = gyros->getData();
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accelData = accels->getData();
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//rawData.gyros[0] = rollRate;
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// Update BaroAltitude object
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//rawData.gyros[1] = cos(DEG2RAD * roll) * pitchRate + sin(DEG2RAD * roll) * yawRate;
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out.temperature = temperature;
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//rawData.gyros[2] = cos(DEG2RAD * roll) * yawRate - sin(DEG2RAD * roll) * pitchRate;
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out.pressure = pressure;
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//rawData.gyros[1] = pitchRate;
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//rawData.gyros[2] = yawRate;
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// Update attActual object
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gyroData.x = rollRate;
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out.roll = roll; //roll;
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gyroData.y = pitchRate;
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out.pitch = pitch; // pitch
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gyroData.z = yawRate;
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out.heading = yaw; // yaw
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// TODO: Accels are still missing!!!!
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gyros->setData(gyroData);
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out.dstN= NED[0];
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// attRaw->updated();
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out.dstE= NED[1];
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out.dstD= NED[2];
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// Update VelocityActual.{North,East,Down}
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out.velNorth = velocityActualNorth;
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out.velEast = velocityActualEast;
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out.velDown = velocityActualDown;
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//Update gyroscope sensor data
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out.rollRate = rollRate;
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out.pitchRate = pitchRate;
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out.yawRate = yawRate;
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//Update accelerometer sensor data
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out.accX = xAccel;
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out.accY = yAccel;
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out.accZ = -zAccel;
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updateUAVOs(out);
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}
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}
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@ -237,127 +237,84 @@ void IL2Simulator::processUpdate(const QByteArray& inp)
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current.dAzimuth = (angleDifference(current.azimuth,old.azimuth)/current.dT + TURN_FILTER * (old.dAzimuth)) / (TURN_FILTER+1);
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current.dAzimuth = (angleDifference(current.azimuth,old.azimuth)/current.dT + TURN_FILTER * (old.dAzimuth)) / (TURN_FILTER+1);
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current.dPitch = (angleDifference(current.pitch,old.pitch)/current.dT + TURN_FILTER * (old.dPitch)) / (TURN_FILTER+1);
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current.dPitch = (angleDifference(current.pitch,old.pitch)/current.dT + TURN_FILTER * (old.dPitch)) / (TURN_FILTER+1);
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current.dRoll = (angleDifference(current.roll,old.roll)/current.dT + TURN_FILTER * (old.dRoll)) / (TURN_FILTER+1);
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current.dRoll = (angleDifference(current.roll,old.roll)/current.dT + TURN_FILTER * (old.dRoll)) / (TURN_FILTER+1);
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// Update AltitudeActual object
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BaroAltitude::DataFields baroAltData;
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memset(&baroAltData, 0, sizeof(BaroAltitude::DataFields));
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baroAltData.Altitude = current.Z;
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baroAltData.Temperature = TEMP_GROUND + (current.Z * TEMP_LAPSE_RATE) - 273.0;
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baroAltData.Pressure = PRESSURE(current.Z)/1000.0; // kpa
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// Update attActual object
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///////
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AttitudeActual::DataFields attActualData;
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// Output formatting
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memset(&attActualData, 0, sizeof(AttitudeActual::DataFields));
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///////
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attActualData.Roll = current.roll;
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Output2OP out;
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attActualData.Pitch = current.pitch;
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memset(&out, 0, sizeof(Output2OP));
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attActualData.Yaw = current.azimuth;
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// Compute rotation matrix, for later calculations
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float Rbe[3][3];
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float rpy[3];
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float rpy[3];
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float quat[4];
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float quat[4];
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rpy[0]=current.roll;
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rpy[0]=current.roll;
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rpy[1]=current.pitch;
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rpy[1]=current.pitch;
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rpy[2]=current.azimuth;
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rpy[2]=current.azimuth;
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Utils::CoordinateConversions().RPY2Quaternion(rpy,quat);
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Utils::CoordinateConversions().RPY2Quaternion(rpy,quat);
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attActualData.q1 = quat[0];
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attActualData.q2 = quat[1];
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attActualData.q3 = quat[2];
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attActualData.q4 = quat[3];
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// Update positionActual objects
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PositionActual::DataFields posData;
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memset(&posData, 0, sizeof(PositionActual::DataFields));
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posData.North = current.Y;
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posData.East = current.X;
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posData.Down = current.Z*-1.;
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// Update velocityActual objects
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VelocityActual::DataFields velData;
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memset(&velData, 0, sizeof(VelocityActual::DataFields));
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velData.North = current.dY;
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velData.East = current.dX;
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velData.Down = current.dZ*-1.;
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// Update AttitudeRaw object (filtered gyros and accels only for now)
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//AttitudeRaw::DataFields rawData;
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//memset(&rawData, 0, sizeof(AttitudeRaw::DataFields));
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//rawData = attRaw->getData();
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Gyros::DataFields gyroData;
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Accels::DataFields accelData;
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memset(&gyroData, 0, sizeof(Gyros::DataFields));
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memset(&accelData, 0, sizeof(Accels::DataFields));
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gyroData = gyros->getData();
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accelData = accels->getData();
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// rotate turn rates and accelerations into body frame
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// (note: rotation deltas are NOT in NED frame but in RPY - manual conversion!)
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gyroData.x = current.dRoll;
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gyroData.y = cos(DEG2RAD * current.roll) * current.dPitch + sin(DEG2RAD * current.roll) * current.dAzimuth;
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gyroData.z = cos(DEG2RAD * current.roll) * current.dAzimuth - sin(DEG2RAD * current.roll) * current.dPitch;
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// accels are in NED and can be converted using standard ned->local rotation matrix
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float Rbe[3][3];
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Utils::CoordinateConversions().Quaternion2R(quat,Rbe);
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Utils::CoordinateConversions().Quaternion2R(quat,Rbe);
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accelData.x = current.ddX*Rbe[0][0]
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+current.ddY*Rbe[0][1]
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+(current.ddZ+GEE)*Rbe[0][2];
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accelData.y = current.ddX*Rbe[1][0]
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+current.ddY*Rbe[1][1]
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+(current.ddZ+GEE)*Rbe[1][2];
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accelData.z = - (current.ddX*Rbe[2][0]
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+current.ddY*Rbe[2][1]
|
|
||||||
+(current.ddZ+GEE)*Rbe[2][2]);
|
|
||||||
|
|
||||||
// Update homelocation
|
//Calculate ECEF
|
||||||
HomeLocation::DataFields homeData;
|
double RNE[9];
|
||||||
memset(&homeData, 0, sizeof(HomeLocation::DataFields));
|
double ECEF[3];
|
||||||
homeData = posHome->getData();
|
|
||||||
homeData.Latitude = settings.latitude.toFloat() * 10e6;
|
|
||||||
homeData.Longitude = settings.longitude.toFloat() * 10e6;
|
|
||||||
homeData.Altitude = 0;
|
|
||||||
double LLA[3];
|
double LLA[3];
|
||||||
LLA[0]=settings.latitude.toFloat();
|
LLA[0]=settings.latitude.toFloat();
|
||||||
LLA[1]=settings.longitude.toFloat();
|
LLA[1]=settings.longitude.toFloat();
|
||||||
LLA[2]=0;
|
LLA[2]=0;
|
||||||
double ECEF[3];
|
|
||||||
double RNE[9];
|
|
||||||
Utils::CoordinateConversions().RneFromLLA(LLA,(double (*)[3])RNE);
|
Utils::CoordinateConversions().RneFromLLA(LLA,(double (*)[3])RNE);
|
||||||
Utils::CoordinateConversions().LLA2ECEF(LLA,ECEF);
|
Utils::CoordinateConversions().LLA2ECEF(LLA,ECEF);
|
||||||
homeData.Be[0]=0;
|
|
||||||
homeData.Be[1]=0;
|
|
||||||
homeData.Be[2]=0;
|
|
||||||
homeData.Set=1;
|
|
||||||
|
|
||||||
// Update gps objects
|
// Update GPS Position objects
|
||||||
GPSPosition::DataFields gpsData;
|
|
||||||
memset(&gpsData, 0, sizeof(GPSPosition::DataFields));
|
|
||||||
gpsData.Altitude = current.Z;
|
|
||||||
gpsData.Heading = current.azimuth;
|
|
||||||
gpsData.Groundspeed = current.groundspeed;
|
|
||||||
double NED[3];
|
double NED[3];
|
||||||
NED[0] = current.Y;
|
NED[0] = current.Y;
|
||||||
NED[1] = current.X;
|
NED[1] = current.X;
|
||||||
NED[2] = -current.Z;
|
NED[2] = -current.Z;
|
||||||
Utils::CoordinateConversions().NED2LLA_HomeECEF(ECEF,NED,LLA);
|
Utils::CoordinateConversions().NED2LLA_HomeECEF(ECEF,NED,LLA);
|
||||||
gpsData.Latitude = LLA[0] * 10e6;
|
out.latitude = settings.latitude.toFloat() * 1e7;
|
||||||
gpsData.Longitude = LLA[1] * 10e6;
|
out.longitude = settings.longitude.toFloat() * 1e7;
|
||||||
gpsData.Satellites = 7;
|
out.groundspeed = current.groundspeed;
|
||||||
gpsData.Status = GPSPosition::STATUS_FIX3D;
|
|
||||||
|
|
||||||
// issue manual update
|
out.calibratedAirspeed = current.ias;
|
||||||
// update every time (50ms)
|
|
||||||
attActual->setData(attActualData);
|
out.dstN=current.Y;
|
||||||
//attActual->updated();
|
out.dstE=current.X;
|
||||||
//attRaw->setData(rawData);
|
out.dstD=-current.Z;
|
||||||
gyros->setData(gyroData);
|
|
||||||
accels->setData(accelData);
|
// Update BaroAltitude object
|
||||||
//attRaw->updated();
|
out.altitude = current.Z;
|
||||||
velActual->setData(velData);
|
out.temperature = TEMP_GROUND + (current.Z * TEMP_LAPSE_RATE) - 273.0;
|
||||||
//velActual->updated();
|
out.pressure = PRESSURE(current.Z)/1000.0; // kpa
|
||||||
posActual->setData(posData);
|
|
||||||
//posActual->updated();
|
|
||||||
baroAlt->setData(baroAltData);
|
// Update attActual object
|
||||||
//baroAlt->updated();
|
out.roll = current.roll; //roll;
|
||||||
gpsPos->setData(gpsData);
|
out.pitch = current.pitch; // pitch
|
||||||
//gpsPos->updated();
|
out.heading = current.azimuth; // yaw
|
||||||
posHome->setData(homeData);
|
|
||||||
//posHome->updated();
|
|
||||||
|
// Update VelocityActual.{North,East,Down}
|
||||||
|
out.velNorth = current.dY;
|
||||||
|
out.velEast = current.dX;
|
||||||
|
out.velDown = -current.dZ;
|
||||||
|
|
||||||
|
// rotate turn rates and accelerations into body frame
|
||||||
|
// (note: rotation deltas are NOT in NED frame but in RPY - manual conversion!)
|
||||||
|
out.rollRate = current.dRoll;
|
||||||
|
out.pitchRate = cos(DEG2RAD * current.roll) * current.dPitch + sin(DEG2RAD * current.roll) * current.dAzimuth;
|
||||||
|
out.yawRate = cos(DEG2RAD * current.roll) * current.dAzimuth - sin(DEG2RAD * current.roll) * current.dPitch;
|
||||||
|
|
||||||
|
//Update accelerometer sensor data
|
||||||
|
out.accX = current.ddX*Rbe[0][0]
|
||||||
|
+current.ddY*Rbe[0][1]
|
||||||
|
+(current.ddZ+GEE)*Rbe[0][2];
|
||||||
|
out.accY = current.ddX*Rbe[1][0]
|
||||||
|
+current.ddY*Rbe[1][1]
|
||||||
|
+(current.ddZ+GEE)*Rbe[1][2];
|
||||||
|
out.accZ = - (current.ddX*Rbe[2][0]
|
||||||
|
+current.ddY*Rbe[2][1]
|
||||||
|
+(current.ddZ+GEE)*Rbe[2][2]);
|
||||||
|
|
||||||
|
updateUAVOs(out);
|
||||||
}
|
}
|
||||||
|
|
||||||
/**
|
/**
|
||||||
|
@ -368,6 +368,11 @@ void Simulator::telStatsUpdated(UAVObject* obj)
|
|||||||
}
|
}
|
||||||
|
|
||||||
|
|
||||||
|
void Simulator::resetInitialHomePosition(){
|
||||||
|
once=false;
|
||||||
|
}
|
||||||
|
|
||||||
|
|
||||||
void Simulator::updateUAVOs(Output2OP out){
|
void Simulator::updateUAVOs(Output2OP out){
|
||||||
|
|
||||||
QTime currentTime = QTime::currentTime();
|
QTime currentTime = QTime::currentTime();
|
||||||
|
@ -25,7 +25,7 @@
|
|||||||
* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
|
* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
|
||||||
*/
|
*/
|
||||||
|
|
||||||
/**
|
/**
|
||||||
* Description of X-Plane Protocol:
|
* Description of X-Plane Protocol:
|
||||||
*
|
*
|
||||||
* To see what data can be sended/recieved to/from X-Plane, launch X-Plane -> goto main menu
|
* To see what data can be sended/recieved to/from X-Plane, launch X-Plane -> goto main menu
|
||||||
@ -68,7 +68,7 @@ void TraceBuf(const char* buf,int len);
|
|||||||
XplaneSimulator::XplaneSimulator(const SimulatorSettings& params) :
|
XplaneSimulator::XplaneSimulator(const SimulatorSettings& params) :
|
||||||
Simulator(params)
|
Simulator(params)
|
||||||
{
|
{
|
||||||
once = false;
|
resetInitialHomePosition();
|
||||||
}
|
}
|
||||||
|
|
||||||
|
|
||||||
@ -82,7 +82,7 @@ void XplaneSimulator::setupUdpPorts(const QString& host, int inPort, int outPort
|
|||||||
|
|
||||||
inSocket->bind(QHostAddress(host), inPort);
|
inSocket->bind(QHostAddress(host), inPort);
|
||||||
//outSocket->bind(QHostAddress(host), outPort);
|
//outSocket->bind(QHostAddress(host), outPort);
|
||||||
once = false;
|
resetInitialHomePosition();
|
||||||
|
|
||||||
}
|
}
|
||||||
|
|
||||||
@ -104,7 +104,7 @@ void XplaneSimulator::transmitUpdate()
|
|||||||
float ailerons = actData.Roll;
|
float ailerons = actData.Roll;
|
||||||
float elevator = actData.Pitch;
|
float elevator = actData.Pitch;
|
||||||
float rudder = actData.Yaw;
|
float rudder = actData.Yaw;
|
||||||
float throttle = actData.Throttle*2-1.0;
|
float throttle = actData.Throttle > 0? actData.Throttle : 0;
|
||||||
float none = -999;
|
float none = -999;
|
||||||
//quint32 none = *((quint32*)&tmp); // get float as 4 bytes
|
//quint32 none = *((quint32*)&tmp); // get float as 4 bytes
|
||||||
|
|
||||||
@ -113,9 +113,9 @@ void XplaneSimulator::transmitUpdate()
|
|||||||
QDataStream stream(&buf,QIODevice::ReadWrite);
|
QDataStream stream(&buf,QIODevice::ReadWrite);
|
||||||
|
|
||||||
// !!! LAN byte order - Big Endian
|
// !!! LAN byte order - Big Endian
|
||||||
#if Q_BYTE_ORDER == Q_LITTLE_ENDIAN
|
#if Q_BYTE_ORDER == Q_LITTLE_ENDIAN
|
||||||
stream.setByteOrder(QDataStream::LittleEndian);
|
stream.setByteOrder(QDataStream::LittleEndian);
|
||||||
#endif
|
#endif
|
||||||
|
|
||||||
// 11th data settings (flight con: ail/elv/rud)
|
// 11th data settings (flight con: ail/elv/rud)
|
||||||
buf.clear();
|
buf.clear();
|
||||||
@ -196,8 +196,8 @@ void XplaneSimulator::processUpdate(const QByteArray& dataBuf)
|
|||||||
float altitude = 0;
|
float altitude = 0;
|
||||||
float latitude = 0;
|
float latitude = 0;
|
||||||
float longitude = 0;
|
float longitude = 0;
|
||||||
float airspeed = 0;
|
float airspeed_keas = 0;
|
||||||
float speed = 0;
|
float groundspeed_ktgs = 0;
|
||||||
float pitch = 0;
|
float pitch = 0;
|
||||||
float roll = 0;
|
float roll = 0;
|
||||||
float heading = 0;
|
float heading = 0;
|
||||||
@ -216,7 +216,7 @@ void XplaneSimulator::processUpdate(const QByteArray& dataBuf)
|
|||||||
float pitchRate_rad=0;
|
float pitchRate_rad=0;
|
||||||
float yawRate_rad=0;
|
float yawRate_rad=0;
|
||||||
|
|
||||||
QString str;
|
// QString str;
|
||||||
QByteArray& buf = const_cast<QByteArray&>(dataBuf);
|
QByteArray& buf = const_cast<QByteArray&>(dataBuf);
|
||||||
QString data(buf);
|
QString data(buf);
|
||||||
|
|
||||||
@ -234,15 +234,15 @@ void XplaneSimulator::processUpdate(const QByteArray& dataBuf)
|
|||||||
{
|
{
|
||||||
switch(buf[0]) // switch by id
|
switch(buf[0]) // switch by id
|
||||||
{
|
{
|
||||||
case XplaneSimulator::LatitudeLongitude:
|
case XplaneSimulator::LatitudeLongitudeAltitude:
|
||||||
latitude = *((float*)(buf.data()+4*1));
|
latitude = *((float*)(buf.data()+4*1));
|
||||||
longitude = *((float*)(buf.data()+4*2));
|
longitude = *((float*)(buf.data()+4*2));
|
||||||
altitude = *((float*)(buf.data()+4*3))* FT2M;
|
altitude = *((float*)(buf.data()+4*3))* FT2M;
|
||||||
break;
|
break;
|
||||||
|
|
||||||
case XplaneSimulator::Speed:
|
case XplaneSimulator::Speed:
|
||||||
airspeed = *((float*)(buf.data()+4*7));
|
airspeed_keas = *((float*)(buf.data()+4*2));
|
||||||
speed = *((float*)(buf.data()+4*8));
|
groundspeed_ktgs = *((float*)(buf.data()+4*4));
|
||||||
break;
|
break;
|
||||||
|
|
||||||
case XplaneSimulator::PitchRollHeading:
|
case XplaneSimulator::PitchRollHeading:
|
||||||
@ -291,125 +291,56 @@ void XplaneSimulator::processUpdate(const QByteArray& dataBuf)
|
|||||||
} while (channelCounter);
|
} while (channelCounter);
|
||||||
|
|
||||||
|
|
||||||
HomeLocation::DataFields homeData = posHome->getData();
|
///////
|
||||||
if(!once)
|
// Output formatting
|
||||||
{
|
///////
|
||||||
// Upon startup, we reset the HomeLocation object to
|
Output2OP out;
|
||||||
// the plane's location:
|
memset(&out, 0, sizeof(Output2OP));
|
||||||
memset(&homeData, 0, sizeof(HomeLocation::DataFields));
|
|
||||||
// Update homelocation
|
|
||||||
homeData.Latitude = latitude * 1e7;
|
|
||||||
homeData.Longitude = longitude * 1e7;
|
|
||||||
homeData.Altitude = altitude;
|
|
||||||
double LLA[3];
|
|
||||||
LLA[0]=latitude;
|
|
||||||
LLA[1]=longitude;
|
|
||||||
LLA[2]=altitude;
|
|
||||||
double ECEF[3];
|
|
||||||
double RNE[9];
|
|
||||||
Utils::CoordinateConversions().RneFromLLA(LLA,(double (*)[3])RNE);
|
|
||||||
Utils::CoordinateConversions().LLA2ECEF(LLA,ECEF);
|
|
||||||
homeData.Be[0]=0;
|
|
||||||
homeData.Be[1]=0;
|
|
||||||
homeData.Be[2]=0;
|
|
||||||
posHome->setData(homeData);
|
|
||||||
posHome->updated();
|
|
||||||
|
|
||||||
// Initialize the initial distance
|
// Update GPS Position objects
|
||||||
initX = dstX;
|
out.latitude = latitude * 1e7;
|
||||||
initY = dstY;
|
out.longitude = longitude * 1e7;
|
||||||
initZ = dstZ;
|
out.altitude = altitude;
|
||||||
once=1;
|
out.groundspeed = groundspeed_ktgs*1.15*1.6089/3.6; //Convert from [kts] to [m/s]
|
||||||
}
|
|
||||||
|
|
||||||
|
out.calibratedAirspeed = airspeed_keas*1.15*1.6089/3.6; //Convert from [kts] to [m/s]
|
||||||
|
|
||||||
// Update AltitudeActual object
|
// Update BaroAltitude object
|
||||||
BaroAltitude::DataFields baroAltData;
|
out.temperature = temperature;
|
||||||
memset(&baroAltData, 0, sizeof(BaroAltitude::DataFields));
|
out.pressure = pressure;
|
||||||
baroAltData.Altitude = altitude;
|
|
||||||
baroAltData.Temperature = temperature;
|
|
||||||
baroAltData.Pressure = pressure;
|
|
||||||
baroAlt->setData(baroAltData);
|
|
||||||
|
|
||||||
// Update attActual object
|
// Update attActual object
|
||||||
AttitudeActual::DataFields attActualData;
|
out.roll = roll; //roll;
|
||||||
memset(&attActualData, 0, sizeof(AttitudeActual::DataFields));
|
out.pitch = pitch; // pitch
|
||||||
attActualData.Roll = roll; //roll;
|
out.heading = heading; // yaw
|
||||||
attActualData.Pitch = pitch; // pitch
|
|
||||||
attActualData.Yaw = heading; // Yaw
|
|
||||||
float rpy[3];
|
|
||||||
float quat[4];
|
|
||||||
rpy[0] = roll;
|
|
||||||
rpy[1] = pitch;
|
|
||||||
rpy[2] = heading;
|
|
||||||
Utils::CoordinateConversions().RPY2Quaternion(rpy,quat);
|
|
||||||
attActualData.q1 = quat[0];
|
|
||||||
attActualData.q2 = quat[1];
|
|
||||||
attActualData.q3 = quat[2];
|
|
||||||
attActualData.q4 = quat[3];
|
|
||||||
attActual->setData(attActualData);
|
|
||||||
|
|
||||||
// Update gps objects
|
|
||||||
GPSPosition::DataFields gpsData;
|
|
||||||
memset(&gpsData, 0, sizeof(GPSPosition::DataFields));
|
|
||||||
gpsData.Altitude = altitude;
|
|
||||||
gpsData.Heading = heading;
|
|
||||||
gpsData.Groundspeed = speed;
|
|
||||||
gpsData.Latitude = latitude*1e7;
|
|
||||||
gpsData.Longitude = longitude*1e7;
|
|
||||||
gpsData.Satellites = 10;
|
|
||||||
gpsData.Status = GPSPosition::STATUS_FIX3D;
|
|
||||||
gpsPos->setData(gpsData);
|
|
||||||
|
|
||||||
// Update VelocityActual.{Nort,East,Down}
|
out.dstN=dstY;
|
||||||
VelocityActual::DataFields velocityActualData;
|
out.dstE=dstX;
|
||||||
memset(&velocityActualData, 0, sizeof(VelocityActual::DataFields));
|
out.dstD=-dstZ;
|
||||||
velocityActualData.North = velY;
|
|
||||||
velocityActualData.East = velX;
|
|
||||||
velocityActualData.Down = -velZ;
|
|
||||||
velActual->setData(velocityActualData);
|
|
||||||
|
|
||||||
// Update PositionActual.{Nort,East,Down}
|
// Update VelocityActual.{North,East,Down}
|
||||||
PositionActual::DataFields positionActualData;
|
out.velNorth = velY;
|
||||||
memset(&positionActualData, 0, sizeof(PositionActual::DataFields));
|
out.velEast = velX;
|
||||||
positionActualData.North = (dstY-initY);
|
out.velDown = -velZ;
|
||||||
positionActualData.East = (dstX-initX);
|
|
||||||
positionActualData.Down = -(dstZ-initZ);
|
|
||||||
posActual->setData(positionActualData);
|
|
||||||
|
|
||||||
// Update AttitudeRaw object (filtered gyros only for now)
|
//Update gyroscope sensor data
|
||||||
//AttitudeRaw::DataFields rawData;
|
out.rollRate = rollRate_rad;
|
||||||
//memset(&rawData, 0, sizeof(AttitudeRaw::DataFields));
|
out.pitchRate = pitchRate_rad;
|
||||||
//rawData = attRaw->getData();
|
out.yawRate = yawRate_rad;
|
||||||
//rawData.gyros[0] = rollRate;
|
|
||||||
//rawData.gyros_filtered[1] = cos(DEG2RAD * roll) * pitchRate_rad + sin(DEG2RAD * roll) * yawRate_rad;
|
|
||||||
//rawData.gyros_filtered[2] = cos(DEG2RAD * roll) * yawRate_rad - sin(DEG2RAD * roll) * pitchRate_rad;
|
|
||||||
//rawData.gyros[1] = pitchRate;
|
|
||||||
//rawData.gyros[2] = yawRate;
|
|
||||||
//rawData.accels[0] = accX;
|
|
||||||
//rawData.accels[1] = accY;
|
|
||||||
//rawData.accels[2] = -accZ;
|
|
||||||
//attRaw->setData(rawData);
|
|
||||||
Gyros::DataFields gyroData;
|
|
||||||
memset(&gyroData, 0, sizeof(Gyros::DataFields));
|
|
||||||
#define Pi 3.141529654
|
|
||||||
gyroData.x = rollRate_rad*180/Pi;
|
|
||||||
gyroData.y = pitchRate_rad*180/Pi;
|
|
||||||
gyroData.z = yawRate_rad*180/Pi;
|
|
||||||
gyros->setData(gyroData);
|
|
||||||
|
|
||||||
Accels::DataFields accelData;
|
//Update accelerometer sensor data
|
||||||
memset(&accelData, 0, sizeof(Accels::DataFields));
|
out.accX = accX;
|
||||||
accelData.x = accX;
|
out.accY = accY;
|
||||||
accelData.y = accY;
|
out.accZ = -accZ;
|
||||||
accelData.z = -accZ;
|
|
||||||
accels->setData(accelData);
|
|
||||||
|
|
||||||
|
updateUAVOs(out);
|
||||||
}
|
}
|
||||||
// issue manual update
|
// issue manual update
|
||||||
//attActual->updated();
|
//attActual->updated();
|
||||||
//baroAlt->updated();
|
//altActual->updated();
|
||||||
//posActual->updated();
|
//posActual->updated();
|
||||||
|
|
||||||
}
|
}
|
||||||
|
|
||||||
|
|
||||||
|
@ -45,12 +45,8 @@ private slots:
|
|||||||
void transmitUpdate();
|
void transmitUpdate();
|
||||||
|
|
||||||
private:
|
private:
|
||||||
bool once;
|
enum XplaneOutputData //***WARNING***: Elements in this enum are in a precise order, do
|
||||||
float initX;
|
{ // not change. Cf. http://www.nuclearprojects.com/xplane/info.shtml
|
||||||
float initY;
|
|
||||||
float initZ;
|
|
||||||
enum XplaneOutputData
|
|
||||||
{
|
|
||||||
FramRate,
|
FramRate,
|
||||||
Times,
|
Times,
|
||||||
SimStats,
|
SimStats,
|
||||||
@ -71,7 +67,7 @@ private:
|
|||||||
AngularVelocities,
|
AngularVelocities,
|
||||||
PitchRollHeading,
|
PitchRollHeading,
|
||||||
AoA,
|
AoA,
|
||||||
LatitudeLongitude,
|
LatitudeLongitudeAltitude,
|
||||||
LocVelDistTraveled
|
LocVelDistTraveled
|
||||||
};
|
};
|
||||||
|
|
||||||
|
Loading…
Reference in New Issue
Block a user