#include "FGAtmosphere.h"
#include "FGFCS.h"
#include "FGAerodynamics.h"
+#include "FGGroundReactions.h"
#include "FGAircraft.h"
#include "FGMassBalance.h"
#include "FGTranslation.h"
#include "FGPosition.h"
#include "FGAuxiliary.h"
+namespace JSBSim {
+
static const char *IdSrc = "$Id$";
static const char *IdHdr = ID_OUTPUT;
-extern short debug_lvl;
-
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CLASS IMPLEMENTATION
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
sFirstPass = dFirstPass = true;
socket = 0;
Type = otNone;
- Filename = "JSBSim.out";
+ Filename = "";
SubSystems = 0;
enabled = true;
+ outputInFileName = "";
-#ifdef FG_WITH_JSBSIM_SOCKET
- socket = new FGfdmSocket("localhost",1138);
-#endif
- if (debug_lvl & 2) cout << "Instantiated: " << Name << endl;
+ Debug(0);
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
FGOutput::~FGOutput()
{
if (socket) delete socket;
- if (debug_lvl & 2) cout << "Destroyed: FGOutput" << endl;
+ for (int i=0; i<OutputProperties.size(); i++) delete OutputProperties[i];
+
+ Debug(1);
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
if (Type == otSocket) {
SocketOutput();
} else if (Type == otCSV) {
- if (Filename != "COUT" && Filename != "cout" && Filename.size() > 0) {
- DelimitedOutput(Filename);
- } else {
- DelimitedOutput();
- }
+ DelimitedOutput(Filename);
} else if (Type == otTerminal) {
// Not done yet
} else if (Type == otNone) {
} else {
// Not a valid type of output
}
-
+ return false;
} else {
+ return true;
}
}
return false;
Type = otSocket;
} else if (type == "TERMINAL") {
Type = otTerminal;
- } else if (type != "NONE"){
+ } else if (type != string("NONE")) {
Type = otUnknown;
cerr << "Unknown type of output specified in config file" << endl;
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGOutput::DelimitedOutput(void)
+void FGOutput::DelimitedOutput(string fname)
{
- if (dFirstPass) {
- cout << "Time";
- if (SubSystems & FGAircraft::ssSimulation) {
- // Nothing here, yet
- }
- if (SubSystems & FGAircraft::ssAerosurfaces) {
- cout << ", ";
- cout << "Throttle, ";
- cout << "Aileron Cmd, ";
- cout << "Elevator Cmd, ";
- cout << "Rudder Cmd, ";
- cout << "Aileron Pos, ";
- cout << "Elevator Pos, ";
- cout << "Rudder Pos";
- }
- if (SubSystems & FGAircraft::ssRates) {
- cout << ", ";
- cout << "P, Q, R";
- }
- if (SubSystems & FGAircraft::ssVelocities) {
- cout << ", ";
- cout << "QBar, ";
- cout << "Vtotal, ";
- cout << "UBody, VBody, WBody, ";
- cout << "UAero, VAero, WAero, ";
- cout << "Vn, Ve, Vd";
- }
- if (SubSystems & FGAircraft::ssForces) {
- cout << ", ";
- cout << "Drag, Side, Lift, ";
- cout << "L/D, ";
- cout << "Xforce, Yforce, Zforce";
- }
- if (SubSystems & FGAircraft::ssMoments) {
- cout << ", ";
- cout << "L, M, N";
- }
- if (SubSystems & FGAircraft::ssAtmosphere) {
- cout << ", ";
- cout << "Rho";
- }
- if (SubSystems & FGAircraft::ssMassProps) {
- cout << ", ";
- cout << "Ixx, ";
- cout << "Iyy, ";
- cout << "Izz, ";
- cout << "Ixz, ";
- cout << "Mass, ";
- cout << "Xcg, Ycg, Zcg";
- }
- if (SubSystems & FGAircraft::ssPosition) {
- cout << ", ";
- cout << "Altitude, ";
- cout << "Phi, Tht, Psi, ";
- cout << "Alpha, ";
- cout << "Latitude, ";
- cout << "Longitude, ";
- cout << "Distance AGL, ";
- cout << "Runway Radius";
- }
- if (SubSystems & FGAircraft::ssCoefficients) {
- cout << ", ";
- cout << Aerodynamics->GetCoefficientStrings();
- }
- if (SubSystems & FGAircraft::ssGroundReactions) {
- cout << ", ";
- cout << Aircraft->GetGroundReactionStrings();
- }
- if (SubSystems & FGAircraft::ssPropulsion) {
- cout << ", ";
- cout << Propulsion->GetPropulsionStrings();
- }
-
- cout << endl;
- dFirstPass = false;
- }
+ streambuf* buffer;
- cout << State->Getsim_time();
- if (SubSystems & FGAircraft::ssSimulation) {
- }
- if (SubSystems & FGAircraft::ssAerosurfaces) {
- cout << ", ";
- cout << FCS->GetThrottlePos(0) << ", ";
- cout << FCS->GetDaCmd() << ", ";
- cout << FCS->GetDeCmd() << ", ";
- cout << FCS->GetDrCmd() << ", ";
- cout << FCS->GetDaPos() << ", ";
- cout << FCS->GetDePos() << ", ";
- cout << FCS->GetDrPos();
- }
- if (SubSystems & FGAircraft::ssRates) {
- cout << ", ";
- cout << Rotation->GetPQR();
- }
- if (SubSystems & FGAircraft::ssVelocities) {
- cout << ", ";
- cout << Translation->Getqbar() << ", ";
- cout << Translation->GetVt() << ", ";
- cout << Translation->GetUVW() << ", ";
- cout << Translation->GetvAero() << ", ";
- cout << Position->GetVel();
- }
- if (SubSystems & FGAircraft::ssForces) {
- cout << ", ";
- cout << Aerodynamics->GetvFs() << ", ";
- cout << Aerodynamics->GetLoD() << ", ";
- cout << Aircraft->GetForces();
- }
- if (SubSystems & FGAircraft::ssMoments) {
- cout << ", ";
- cout << Aircraft->GetMoments();
- }
- if (SubSystems & FGAircraft::ssAtmosphere) {
- cout << ", ";
- cout << Atmosphere->GetDensity();
- }
- if (SubSystems & FGAircraft::ssMassProps) {
- cout << ", ";
- cout << MassBalance->GetIxx() << ", ";
- cout << MassBalance->GetIyy() << ", ";
- cout << MassBalance->GetIzz() << ", ";
- cout << MassBalance->GetIxz() << ", ";
- cout << MassBalance->GetMass() << ", ";
- cout << MassBalance->GetXYZcg();
- }
- if (SubSystems & FGAircraft::ssPosition) {
- cout << ", ";
- cout << Position->Geth() << ", ";
- cout << Rotation->GetEuler() << ", ";
- cout << Translation->Getalpha() << ", ";
- cout << Position->GetLatitude() << ", ";
- cout << Position->GetLongitude() << ", ";
- cout << Position->GetDistanceAGL() << ", ";
- cout << Position->GetRunwayRadius();
- }
- if (SubSystems & FGAircraft::ssCoefficients) {
- cout << ", ";
- cout << Aerodynamics->GetCoefficientValues();
- }
- if (SubSystems & FGAircraft::ssGroundReactions) {
- cout << ", ";
- cout << Aircraft->GetGroundReactionValues();
- }
- if (SubSystems & FGAircraft::ssPropulsion) {
- cout << ", ";
- cout << Propulsion->GetPropulsionValues();
+ if (fname == "COUT" || fname == "cout") {
+ buffer = cout.rdbuf();
+ } else {
+ datafile.open(fname.c_str());
+ buffer = datafile.rdbuf();
}
- cout << endl;
-}
+ ostream outstream(buffer);
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-void FGOutput::DelimitedOutput(string fname)
-{
- if (sFirstPass) {
- datafile.open(fname.c_str());
- datafile << "Time";
- if (SubSystems & FGAircraft::ssSimulation) {
+ if (dFirstPass) {
+ outstream << "Time";
+ if (SubSystems & ssSimulation) {
// Nothing here, yet
}
- if (SubSystems & FGAircraft::ssAerosurfaces) {
- datafile << ", ";
- datafile << "Throttle, ";
- datafile << "Aileron Cmd, ";
- datafile << "Elevator Cmd, ";
- datafile << "Rudder Cmd, ";
- datafile << "Aileron Pos, ";
- datafile << "Elevator Pos, ";
- datafile << "Rudder Pos";
- }
- if (SubSystems & FGAircraft::ssRates) {
- datafile << ", ";
- datafile << "P, Q, R";
- }
- if (SubSystems & FGAircraft::ssVelocities) {
- datafile << ", ";
- datafile << "QBar, ";
- datafile << "Vtotal, ";
- datafile << "UBody, VBody, WBody, ";
- datafile << "UAero, VAero, WAero, ";
- datafile << "Vn, Ve, Vd";
- }
- if (SubSystems & FGAircraft::ssForces) {
- datafile << ", ";
- datafile << "Drag, Side, Lift, ";
- datafile << "L/D, ";
- datafile << "Xforce, Yforce, Zforce";
- }
- if (SubSystems & FGAircraft::ssMoments) {
- datafile << ", ";
- datafile << "L, M, N";
- }
- if (SubSystems & FGAircraft::ssAtmosphere) {
- datafile << ", ";
- datafile << "Rho";
- }
- if (SubSystems & FGAircraft::ssMassProps) {
- datafile << ", ";
- datafile << "Ixx, ";
- datafile << "Iyy, ";
- datafile << "Izz, ";
- datafile << "Ixz, ";
- datafile << "Mass, ";
- datafile << "Xcg, Ycg, Zcg";
- }
- if (SubSystems & FGAircraft::ssPosition) {
- datafile << ", ";
- datafile << "Altitude, ";
- datafile << "Phi, Tht, Psi, ";
- datafile << "Alpha, ";
- datafile << "Latitude, ";
- datafile << "Longitude, ";
- datafile << "Distance AGL, ";
- datafile << "Runway Radius";
- }
- if (SubSystems & FGAircraft::ssCoefficients) {
- datafile << ", ";
- datafile << Aerodynamics->GetCoefficientStrings();
- }
- if (SubSystems & FGAircraft::ssGroundReactions) {
- datafile << ", ";
- datafile << Aircraft->GetGroundReactionStrings();
- }
- if (SubSystems & FGAircraft::ssFCS) {
- datafile << ", ";
- datafile << FCS->GetComponentStrings();
- }
- if (SubSystems & FGAircraft::ssPropulsion) {
- datafile << ", ";
- datafile << Propulsion->GetPropulsionStrings();
- }
- datafile << endl;
- sFirstPass = false;
+ if (SubSystems & ssAerosurfaces) {
+ outstream << ", ";
+ outstream << "Aileron Cmd, ";
+ outstream << "Elevator Cmd, ";
+ outstream << "Rudder Cmd, ";
+ outstream << "Flap Cmd, ";
+ outstream << "Left Aileron Pos, ";
+ outstream << "Right Aileron Pos, ";
+ outstream << "Elevator Pos, ";
+ outstream << "Rudder Pos, ";
+ outstream << "Flap Pos";
+ }
+ if (SubSystems & ssRates) {
+ outstream << ", ";
+ outstream << "P, Q, R, ";
+ outstream << "Pdot, Qdot, Rdot";
+ }
+ if (SubSystems & ssVelocities) {
+ outstream << ", ";
+ outstream << "QBar, ";
+ outstream << "Vtotal, ";
+ outstream << "UBody, VBody, WBody, ";
+ outstream << "UAero, VAero, WAero, ";
+ outstream << "Vn, Ve, Vd";
+ }
+ if (SubSystems & ssForces) {
+ outstream << ", ";
+ outstream << "Drag, Side, Lift, ";
+ outstream << "L/D, ";
+ outstream << "Xforce, Yforce, Zforce, ";
+ outstream << "xGravity, yGravity, zGravity, ";
+ outstream << "xCoriolis, yCoriolis, zCoriolis, ";
+ outstream << "xCentrifugal, yCentrifugal, zCentrifugal";
+ }
+ if (SubSystems & ssMoments) {
+ outstream << ", ";
+ outstream << "L, M, N";
+ }
+ if (SubSystems & ssAtmosphere) {
+ outstream << ", ";
+ outstream << "Rho, ";
+ outstream << "NWind, EWind, DWind";
+ }
+ if (SubSystems & ssMassProps) {
+ outstream << ", ";
+ outstream << "Ixx, ";
+ outstream << "Iyy, ";
+ outstream << "Izz, ";
+ outstream << "Ixz, ";
+ outstream << "Mass, ";
+ outstream << "Xcg, Ycg, Zcg";
+ }
+ if (SubSystems & ssPosition) {
+ outstream << ", ";
+ outstream << "Altitude, ";
+ outstream << "Phi, Tht, Psi, ";
+ outstream << "Alpha, ";
+ outstream << "Beta, ";
+ outstream << "Latitude, ";
+ outstream << "Longitude, ";
+ outstream << "Distance AGL, ";
+ outstream << "Runway Radius";
+ }
+ if (SubSystems & ssCoefficients) {
+ outstream << ", ";
+ outstream << Aerodynamics->GetCoefficientStrings();
+ }
+ if (SubSystems & ssFCS) {
+ outstream << ", ";
+ outstream << FCS->GetComponentStrings();
+ }
+ if (SubSystems & ssGroundReactions) {
+ outstream << ", ";
+ outstream << GroundReactions->GetGroundReactionStrings();
+ }
+ if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
+ outstream << ", ";
+ outstream << Propulsion->GetPropulsionStrings();
+ }
+ if (OutputProperties.size() > 0) {
+ for (int i=0;i<OutputProperties.size();i++) {
+ outstream << ", " << OutputProperties[i]->GetName();
+ }
+ }
+
+ outstream << endl;
+ dFirstPass = false;
}
- datafile << State->Getsim_time();
- if (SubSystems & FGAircraft::ssSimulation) {
+ outstream << State->Getsim_time();
+ if (SubSystems & ssSimulation) {
}
- if (SubSystems & FGAircraft::ssAerosurfaces) {
- datafile << ", ";
- datafile << FCS->GetThrottlePos(0) << ", ";
- datafile << FCS->GetDaCmd() << ", ";
- datafile << FCS->GetDeCmd() << ", ";
- datafile << FCS->GetDrCmd() << ", ";
- datafile << FCS->GetDaPos() << ", ";
- datafile << FCS->GetDePos() << ", ";
- datafile << FCS->GetDrPos();
+ if (SubSystems & ssAerosurfaces) {
+ outstream << ", ";
+ outstream << FCS->GetDaCmd() << ", ";
+ outstream << FCS->GetDeCmd() << ", ";
+ outstream << FCS->GetDrCmd() << ", ";
+ outstream << FCS->GetDfCmd() << ", ";
+ outstream << FCS->GetDaLPos() << ", ";
+ outstream << FCS->GetDaRPos() << ", ";
+ outstream << FCS->GetDePos() << ", ";
+ outstream << FCS->GetDrPos() << ", ";
+ outstream << FCS->GetDfPos();
}
- if (SubSystems & FGAircraft::ssRates) {
- datafile << ", ";
- datafile << Rotation->GetPQR();
+ if (SubSystems & ssRates) {
+ outstream << ", ";
+ outstream << Rotation->GetPQR() << ", ";
+ outstream << Rotation->GetPQRdot();
}
- if (SubSystems & FGAircraft::ssVelocities) {
- datafile << ", ";
- datafile << Translation->Getqbar() << ", ";
- datafile << Translation->GetVt() << ", ";
- datafile << Translation->GetUVW() << ", ";
- datafile << Translation->GetvAero() << ", ";
- datafile << Position->GetVel();
+ if (SubSystems & ssVelocities) {
+ outstream << ", ";
+ outstream << Translation->Getqbar() << ", ";
+ outstream << Translation->GetVt() << ", ";
+ outstream << Translation->GetUVW() << ", ";
+ outstream << Translation->GetAeroUVW() << ", ";
+ outstream << Position->GetVel();
}
- if (SubSystems & FGAircraft::ssForces) {
- datafile << ", ";
- datafile << Aerodynamics->GetvFs() << ", ";
- datafile << Aerodynamics->GetLoD() << ", ";
- datafile << Aircraft->GetForces();
+ if (SubSystems & ssForces) {
+ outstream << ", ";
+ outstream << Aerodynamics->GetvFs() << ", ";
+ outstream << Aerodynamics->GetLoD() << ", ";
+ outstream << Aircraft->GetForces() << ", ";
+ outstream << Inertial->GetGravity() << ", ";
+ outstream << Inertial->GetCoriolis() << ", ";
+ outstream << Inertial->GetCentrifugal();
}
- if (SubSystems & FGAircraft::ssMoments) {
- datafile << ", ";
- datafile << Aircraft->GetMoments();
+ if (SubSystems & ssMoments) {
+ outstream << ", ";
+ outstream << Aircraft->GetMoments();
}
- if (SubSystems & FGAircraft::ssAtmosphere) {
- datafile << ", ";
- datafile << Atmosphere->GetDensity();
+ if (SubSystems & ssAtmosphere) {
+ outstream << ", ";
+ outstream << Atmosphere->GetDensity() << ", ";
+ outstream << Atmosphere->GetWindNED();
}
- if (SubSystems & FGAircraft::ssMassProps) {
- datafile << ", ";
- datafile << MassBalance->GetIxx() << ", ";
- datafile << MassBalance->GetIyy() << ", ";
- datafile << MassBalance->GetIzz() << ", ";
- datafile << MassBalance->GetIxz() << ", ";
- datafile << MassBalance->GetMass() << ", ";
- datafile << MassBalance->GetXYZcg();
+ if (SubSystems & ssMassProps) {
+ outstream << ", ";
+ outstream << MassBalance->GetIxx() << ", ";
+ outstream << MassBalance->GetIyy() << ", ";
+ outstream << MassBalance->GetIzz() << ", ";
+ outstream << MassBalance->GetIxz() << ", ";
+ outstream << MassBalance->GetMass() << ", ";
+ outstream << MassBalance->GetXYZcg();
}
- if (SubSystems & FGAircraft::ssPosition) {
- datafile << ", ";
- datafile << Position->Geth() << ", ";
- datafile << Rotation->GetEuler() << ", ";
- datafile << Translation->Getalpha() << ", ";
- datafile << Position->GetLatitude() << ", ";
- datafile << Position->GetLongitude() << ", ";
- datafile << Position->GetDistanceAGL() << ", ";
- datafile << Position->GetRunwayRadius();
+ if (SubSystems & ssPosition) {
+ outstream << ", ";
+ outstream << Position->Geth() << ", ";
+ outstream << Rotation->GetEuler() << ", ";
+ outstream << Translation->Getalpha() << ", ";
+ outstream << Translation->Getbeta() << ", ";
+ outstream << Position->GetLatitude() << ", ";
+ outstream << Position->GetLongitude() << ", ";
+ outstream << Position->GetDistanceAGL() << ", ";
+ outstream << Position->GetRunwayRadius();
}
- if (SubSystems & FGAircraft::ssCoefficients) {
- datafile << ", ";
- datafile << Aerodynamics->GetCoefficientValues();
+ if (SubSystems & ssCoefficients) {
+ outstream << ", ";
+ outstream << Aerodynamics->GetCoefficientValues();
}
- if (SubSystems & FGAircraft::ssGroundReactions) {
- datafile << ", ";
- datafile << Aircraft->GetGroundReactionValues();
+ if (SubSystems & ssFCS) {
+ outstream << ", ";
+ outstream << FCS->GetComponentValues();
}
- if (SubSystems & FGAircraft::ssFCS) {
- datafile << ", ";
- datafile << FCS->GetComponentValues();
+ if (SubSystems & ssGroundReactions) {
+ outstream << ", ";
+ outstream << GroundReactions->GetGroundReactionValues();
}
- if (SubSystems & FGAircraft::ssPropulsion) {
- datafile << ", ";
- datafile << Propulsion->GetPropulsionValues();
+ if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
+ outstream << ", ";
+ outstream << Propulsion->GetPropulsionValues();
}
- datafile << endl;
- datafile.flush();
+
+ for (int i=0;i<OutputProperties.size();i++) {
+ outstream << ", " << OutputProperties[i]->getDoubleValue();
+ }
+
+ outstream << endl;
+ outstream.flush();
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGOutput::SocketOutput(void)
{
string asciiData;
- /*
+
if (socket == NULL) return;
+ if (!socket->GetConnectStatus()) return;
socket->Clear();
if (sFirstPass) {
socket->Append("L");
socket->Append("M");
socket->Append("N");
- socket->Append("Throttle");
- socket->Append("Aileron");
- socket->Append("Elevator");
- socket->Append("Rudder");
+ socket->Append("Throttle Position");
+ socket->Append("Left Aileron Position");
+ socket->Append("Right Aileron Position");
+ socket->Append("Elevator Position");
+ socket->Append("Rudder Position");
sFirstPass = false;
socket->Send();
}
socket->Append(Translation->GetUVW(eU));
socket->Append(Translation->GetUVW(eV));
socket->Append(Translation->GetUVW(eW));
- socket->Append(Translation->GetvAero(eU));
- socket->Append(Translation->GetvAero(eV));
- socket->Append(Translation->GetvAero(eW));
+ socket->Append(Translation->GetAeroUVW(eU));
+ socket->Append(Translation->GetAeroUVW(eV));
+ socket->Append(Translation->GetAeroUVW(eW));
socket->Append(Position->GetVn());
socket->Append(Position->GetVe());
socket->Append(Position->GetVd());
- socket->Append(Translation->GetUdot());
- socket->Append(Translation->GetVdot());
- socket->Append(Translation->GetWdot());
- socket->Append(Rotation->GetP());
- socket->Append(Rotation->GetQ());
- socket->Append(Rotation->GetR());
- socket->Append(Rotation->GetPdot());
- socket->Append(Rotation->GetQdot());
- socket->Append(Rotation->GetRdot());
- socket->Append(Aircraft->GetFx());
- socket->Append(Aircraft->GetFy());
- socket->Append(Aircraft->GetFz());
+ socket->Append(Translation->GetUVWdot(eU));
+ socket->Append(Translation->GetUVWdot(eV));
+ socket->Append(Translation->GetUVWdot(eW));
+ socket->Append(Rotation->GetPQR(eP));
+ socket->Append(Rotation->GetPQR(eQ));
+ socket->Append(Rotation->GetPQR(eR));
+ socket->Append(Rotation->GetPQRdot(eP));
+ socket->Append(Rotation->GetPQRdot(eQ));
+ socket->Append(Rotation->GetPQRdot(eR));
+ socket->Append(Aircraft->GetForces(eX));
+ socket->Append(Aircraft->GetForces(eY));
+ socket->Append(Aircraft->GetForces(eZ));
socket->Append(Position->GetLatitude());
socket->Append(Position->GetLongitude());
socket->Append(Translation->Getqbar());
socket->Append(Translation->Getalpha());
- socket->Append(Aircraft->GetL());
- socket->Append(Aircraft->GetM());
- socket->Append(Aircraft->GetN());
- socket->Append(FCS->GetThrottle(0));
- socket->Append(FCS->GetDa());
- socket->Append(FCS->GetDe());
- socket->Append(FCS->GetDr());
- socket->Send(); */
+ socket->Append(Aircraft->GetMoments(eL));
+ socket->Append(Aircraft->GetMoments(eM));
+ socket->Append(Aircraft->GetMoments(eN));
+ socket->Append(FCS->GetThrottlePos(0));
+ socket->Append(FCS->GetDaLPos());
+ socket->Append(FCS->GetDaRPos());
+ socket->Append(FCS->GetDePos());
+ socket->Append(FCS->GetDrPos());
+ socket->Send();
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGOutput::Debug(void)
+bool FGOutput::Load(FGConfigFile* AC_cfg)
{
- //TODO: Add your source code here
+ string token="", parameter="", separator="";
+ string name="", fname="";
+ int OutRate = 0;
+ FGConfigFile* Output_cfg;
+ string property;
+
+# ifndef macintosh
+ separator = "/";
+# else
+ separator = ";";
+# endif
+
+ name = AC_cfg->GetValue("NAME");
+ fname = AC_cfg->GetValue("FILE");
+ token = AC_cfg->GetValue("TYPE");
+ Output->SetType(token);
+
+#if defined( FG_WITH_JSBSIM_SOCKET ) || !defined( FGFS )
+ if (token == "SOCKET") {
+ socket = new FGfdmSocket("localhost",1138);
+ }
+#endif
+
+ if (!fname.empty()) {
+ outputInFileName = FDMExec->GetAircraftPath() + separator
+ + FDMExec->GetModelName() + separator + fname + ".xml";
+ Output_cfg = new FGConfigFile(outputInFileName);
+ if (!Output_cfg->IsOpen()) {
+ cerr << "Could not open file: " << outputInFileName << endl;
+ return false;
+ }
+ } else {
+ Output_cfg = AC_cfg;
+ }
+ Output->SetFilename(name);
+
+ while ((token = Output_cfg->GetValue()) != string("/OUTPUT")) {
+ *Output_cfg >> parameter;
+ if (parameter == "RATE_IN_HZ") {
+ *Output_cfg >> OutRate;
+ }
+ if (parameter == "SIMULATION") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssSimulation;
+ }
+ if (parameter == "AEROSURFACES") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssAerosurfaces;
+ }
+ if (parameter == "RATES") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssRates;
+ }
+ if (parameter == "VELOCITIES") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssVelocities;
+ }
+ if (parameter == "FORCES") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssForces;
+ }
+ if (parameter == "MOMENTS") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssMoments;
+ }
+ if (parameter == "ATMOSPHERE") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssAtmosphere;
+ }
+ if (parameter == "MASSPROPS") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssMassProps;
+ }
+ if (parameter == "POSITION") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssPosition;
+ }
+ if (parameter == "COEFFICIENTS") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssCoefficients;
+ }
+ if (parameter == "GROUND_REACTIONS") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssGroundReactions;
+ }
+ if (parameter == "FCS") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssFCS;
+ }
+ if (parameter == "PROPULSION") {
+ *Output_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssPropulsion;
+ }
+ if (parameter == "PROPERTY") {
+ *Output_cfg >> property;
+ OutputProperties.push_back(PropertyManager->GetNode(property));
+ }
+
+ if (parameter == "EOF") break;
+ }
+
+ OutRate = OutRate>120?120:(OutRate<0?0:OutRate);
+ rate = (int)(0.5 + 1.0/(State->Getdt()*OutRate));
+
+ Debug(2);
+
+ return true;
}
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+// The bitmasked value choices are as follows:
+// unset: In this case (the default) JSBSim would only print
+// out the normally expected messages, essentially echoing
+// the config files as they are read. If the environment
+// variable is not set, debug_lvl is set to 1 internally
+// 0: This requests JSBSim not to output any messages
+// whatsoever.
+// 1: This value explicity requests the normal JSBSim
+// startup messages
+// 2: This value asks for a message to be printed out when
+// a class is instantiated
+// 4: When this value is set, a message is displayed when a
+// FGModel object executes its Run() method
+// 8: When this value is set, various runtime state variables
+// are printed out periodically
+// 16: When set various parameters are sanity checked and
+// a message is printed out when they go out of bounds
+
+void FGOutput::Debug(int from)
+{
+ string scratch="";
+
+ if (debug_lvl <= 0) return;
+
+ if (debug_lvl & 1) { // Standard console startup message output
+ if (from == 0) { // Constructor
+
+ }
+ if (from == 2) {
+ if (outputInFileName.empty())
+ cout << " " << "Output parameters read inline" << endl;
+ else
+ cout << " Output parameters read from file: " << outputInFileName << endl;
+
+ if (Filename == "cout" || Filename == "COUT") {
+ scratch = " Log output goes to screen console";
+ } else if (!Filename.empty()) {
+ scratch = " Log output goes to file: " + Filename;
+ }
+ switch (Type) {
+ case otCSV:
+ cout << scratch << " in CSV format output at rate " << 120/rate << " Hz" << endl;
+ break;
+ case otNone:
+ cout << " No log output" << endl;
+ break;
+ }
+
+ if (SubSystems & ssSimulation) cout << " Simulation parameters logged" << endl;
+ if (SubSystems & ssAerosurfaces) cout << " Aerosurface parameters logged" << endl;
+ if (SubSystems & ssRates) cout << " Rate parameters logged" << endl;
+ if (SubSystems & ssVelocities) cout << " Velocity parameters logged" << endl;
+ if (SubSystems & ssForces) cout << " Force parameters logged" << endl;
+ if (SubSystems & ssMoments) cout << " Moments parameters logged" << endl;
+ if (SubSystems & ssAtmosphere) cout << " Atmosphere parameters logged" << endl;
+ if (SubSystems & ssMassProps) cout << " Mass parameters logged" << endl;
+ if (SubSystems & ssCoefficients) cout << " Coefficient parameters logged" << endl;
+ if (SubSystems & ssPosition) cout << " Position parameters logged" << endl;
+ if (SubSystems & ssGroundReactions) cout << " Ground parameters logged" << endl;
+ if (SubSystems & ssFCS) cout << " FCS parameters logged" << endl;
+ if (SubSystems & ssPropulsion) cout << " Propulsion parameters logged" << endl;
+ }
+ }
+ if (debug_lvl & 2 ) { // Instantiation/Destruction notification
+ if (from == 0) cout << "Instantiated: FGOutput" << endl;
+ if (from == 1) cout << "Destroyed: FGOutput" << endl;
+ }
+ if (debug_lvl & 4 ) { // Run() method entry print for FGModel-derived objects
+ }
+ if (debug_lvl & 8 ) { // Runtime state variables
+ }
+ if (debug_lvl & 16) { // Sanity checking
+ }
+ if (debug_lvl & 64) {
+ if (from == 0) { // Constructor
+ cout << IdSrc << endl;
+ cout << IdHdr << endl;
+ }
+ }
+}
+}
projects / flightgear.git / blobdiff