SubSystems = 0;
enabled = true;
-#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;
+ Debug(1);
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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(string fname)
{
-# if defined(sgi) && !defined(__GNUC__)
- ostream_withassign outstream;
-# else
- _IO_ostream_withassign outstream;
-# endif
+ streambuf* buffer;
if (fname == "COUT" || fname == "cout") {
- outstream = cout;
+ buffer = cout.rdbuf();
} else {
datafile.open(fname.c_str());
- outstream = datafile;
+ buffer = datafile.rdbuf();
}
+ ostream outstream(buffer);
+
if (dFirstPass) {
outstream << "Time";
- if (SubSystems & FGAircraft::ssSimulation) {
+ if (SubSystems & ssSimulation) {
// Nothing here, yet
}
- if (SubSystems & FGAircraft::ssAerosurfaces) {
+ if (SubSystems & ssAerosurfaces) {
outstream << ", ";
- outstream << "Throttle, ";
- outstream << "Mixture, ";
outstream << "Aileron Cmd, ";
outstream << "Elevator Cmd, ";
outstream << "Rudder Cmd, ";
outstream << "Elevator Pos, ";
outstream << "Rudder Pos";
}
- if (SubSystems & FGAircraft::ssRates) {
+ if (SubSystems & ssRates) {
outstream << ", ";
- outstream << "P, Q, R";
+ outstream << "P, Q, R, ";
+ outstream << "Pdot, Qdot, Rdot";
}
- if (SubSystems & FGAircraft::ssVelocities) {
+ if (SubSystems & ssVelocities) {
outstream << ", ";
outstream << "QBar, ";
outstream << "Vtotal, ";
outstream << "UAero, VAero, WAero, ";
outstream << "Vn, Ve, Vd";
}
- if (SubSystems & FGAircraft::ssForces) {
+ if (SubSystems & ssForces) {
outstream << ", ";
outstream << "Drag, Side, Lift, ";
outstream << "L/D, ";
outstream << "Xforce, Yforce, Zforce";
}
- if (SubSystems & FGAircraft::ssMoments) {
+ if (SubSystems & ssMoments) {
outstream << ", ";
outstream << "L, M, N";
}
- if (SubSystems & FGAircraft::ssAtmosphere) {
+ if (SubSystems & ssAtmosphere) {
outstream << ", ";
- outstream << "Rho";
+ outstream << "Rho, ";
+ outstream << "NWind, EWind, DWind";
}
- if (SubSystems & FGAircraft::ssMassProps) {
+ if (SubSystems & ssMassProps) {
outstream << ", ";
outstream << "Ixx, ";
outstream << "Iyy, ";
outstream << "Mass, ";
outstream << "Xcg, Ycg, Zcg";
}
- if (SubSystems & FGAircraft::ssPosition) {
+ 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 & FGAircraft::ssCoefficients) {
+ if (SubSystems & ssCoefficients) {
outstream << ", ";
outstream << Aerodynamics->GetCoefficientStrings();
}
- if (SubSystems & FGAircraft::ssGroundReactions) {
+ if (SubSystems & ssGroundReactions) {
outstream << ", ";
outstream << GroundReactions->GetGroundReactionStrings();
}
- if (SubSystems & FGAircraft::ssPropulsion) {
+ if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
outstream << ", ";
outstream << Propulsion->GetPropulsionStrings();
}
}
outstream << State->Getsim_time();
- if (SubSystems & FGAircraft::ssSimulation) {
+ if (SubSystems & ssSimulation) {
}
- if (SubSystems & FGAircraft::ssAerosurfaces) {
+ if (SubSystems & ssAerosurfaces) {
outstream << ", ";
- outstream << FCS->GetThrottlePos(0) << ", ";
- outstream << FCS->GetMixturePos(0) << ", ";
outstream << FCS->GetDaCmd() << ", ";
outstream << FCS->GetDeCmd() << ", ";
outstream << FCS->GetDrCmd() << ", ";
outstream << FCS->GetDePos() << ", ";
outstream << FCS->GetDrPos();
}
- if (SubSystems & FGAircraft::ssRates) {
+ if (SubSystems & ssRates) {
outstream << ", ";
- outstream << Rotation->GetPQR();
+ outstream << Rotation->GetPQR() << ", ";
+ outstream << Rotation->GetPQRdot();
}
- if (SubSystems & FGAircraft::ssVelocities) {
+ if (SubSystems & ssVelocities) {
outstream << ", ";
outstream << Translation->Getqbar() << ", ";
outstream << Translation->GetVt() << ", ";
outstream << Translation->GetUVW() << ", ";
- outstream << Translation->GetvAero() << ", ";
+ outstream << Translation->GetvAeroUVW() << ", ";
outstream << Position->GetVel();
}
- if (SubSystems & FGAircraft::ssForces) {
+ if (SubSystems & ssForces) {
outstream << ", ";
outstream << Aerodynamics->GetvFs() << ", ";
outstream << Aerodynamics->GetLoD() << ", ";
outstream << Aircraft->GetForces();
}
- if (SubSystems & FGAircraft::ssMoments) {
+ if (SubSystems & ssMoments) {
outstream << ", ";
outstream << Aircraft->GetMoments();
}
- if (SubSystems & FGAircraft::ssAtmosphere) {
+ if (SubSystems & ssAtmosphere) {
outstream << ", ";
- outstream << Atmosphere->GetDensity();
+ outstream << Atmosphere->GetDensity() << ", ";
+ outstream << Atmosphere->GetWindNED();
}
- if (SubSystems & FGAircraft::ssMassProps) {
+ if (SubSystems & ssMassProps) {
outstream << ", ";
outstream << MassBalance->GetIxx() << ", ";
outstream << MassBalance->GetIyy() << ", ";
outstream << MassBalance->GetMass() << ", ";
outstream << MassBalance->GetXYZcg();
}
- if (SubSystems & FGAircraft::ssPosition) {
+ 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) {
+ if (SubSystems & ssCoefficients) {
outstream << ", ";
outstream << Aerodynamics->GetCoefficientValues();
}
- if (SubSystems & FGAircraft::ssGroundReactions) {
+ if (SubSystems & ssGroundReactions) {
outstream << ", ";
outstream << GroundReactions->GetGroundReactionValues();
}
- if (SubSystems & FGAircraft::ssPropulsion) {
+ if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
outstream << ", ";
outstream << Propulsion->GetPropulsionValues();
}
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("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->GetvAeroUVW(eU));
+ socket->Append(Translation->GetvAeroUVW(eV));
+ socket->Append(Translation->GetvAeroUVW(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->GetDaPos());
+ 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;
+ int OutRate = 0;
+
+ token = AC_cfg->GetValue("NAME");
+ Output->SetFilename(token);
+ 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
+
+ AC_cfg->GetNextConfigLine();
+
+ while ((token = AC_cfg->GetValue()) != string("/OUTPUT")) {
+ *AC_cfg >> parameter;
+ if (parameter == "RATE_IN_HZ") *AC_cfg >> OutRate;
+ if (parameter == "SIMULATION") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssSimulation;
+ }
+ if (parameter == "AEROSURFACES") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssAerosurfaces;
+ }
+ if (parameter == "RATES") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssRates;
+ }
+ if (parameter == "VELOCITIES") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssVelocities;
+ }
+ if (parameter == "FORCES") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssForces;
+ }
+ if (parameter == "MOMENTS") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssMoments;
+ }
+ if (parameter == "ATMOSPHERE") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssAtmosphere;
+ }
+ if (parameter == "MASSPROPS") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssMassProps;
+ }
+ if (parameter == "POSITION") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssPosition;
+ }
+ if (parameter == "COEFFICIENTS") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssCoefficients;
+ }
+ if (parameter == "GROUND_REACTIONS") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssGroundReactions;
+ }
+ if (parameter == "FCS") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssFCS;
+ }
+ if (parameter == "PROPULSION") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") SubSystems += ssPropulsion;
+ }
+ }
+
+ OutRate = OutRate>120?120:(OutRate<0?0:OutRate);
+ rate = (int)(0.5 + 1.0/(State->Getdt()*OutRate));
+
+ 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)
+{
+ if (debug_lvl <= 0) return;
+
+ if (debug_lvl & 1) { // Standard console startup message output
+ if (from == 0) { // Constructor
+
+ }
+ }
+ 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