FUNCTIONAL DESCRIPTION
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This is the place where you create output routines to dump data for perusal
-later.
+later.
HISTORY
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#include "FGGroundReactions.h"
#include "FGAircraft.h"
#include "FGMassBalance.h"
-#include "FGTranslation.h"
-#include "FGRotation.h"
-#include "FGPosition.h"
+#include "FGPropagate.h"
#include "FGAuxiliary.h"
+#include "FGInertial.h"
+
+#include <iomanip>
namespace JSBSim {
SubSystems = 0;
enabled = true;
outputInFileName = "";
-
+ delimeter = ", ";
+
Debug(0);
}
FGOutput::~FGOutput()
{
if (socket) delete socket;
- for (int i=0; i<OutputProperties.size(); i++) delete OutputProperties[i];
+ for (unsigned int i=0; i<OutputProperties.size(); i++) delete OutputProperties[i];
Debug(1);
}
bool FGOutput::Run(void)
{
if (enabled) {
- if (!FGModel::Run()) {
-
- if (Type == otSocket) {
- SocketOutput();
- } else if (Type == otCSV) {
- DelimitedOutput(Filename);
- } else if (Type == otTerminal) {
- // Not done yet
- } else if (Type == otNone) {
- // Do nothing
- } else {
- // Not a valid type of output
- }
- return false;
+ if (FGModel::Run()) return true;
+ if (Type == otSocket) {
+ SocketOutput();
+ } else if (Type == otCSV || Type == otTab) {
+ DelimitedOutput(Filename);
+ } else if (Type == otTerminal) {
+ // Not done yet
+ } else if (Type == otNone) {
+ // Do nothing
} else {
- return true;
+ // Not a valid type of output
}
}
return false;
{
if (type == "CSV") {
Type = otCSV;
+ delimeter = ", ";
} else if (type == "TABULAR") {
Type = otTab;
+ delimeter = "\t";
} else if (type == "SOCKET") {
Type = otSocket;
} else if (type == "TERMINAL") {
void FGOutput::DelimitedOutput(string fname)
{
streambuf* buffer;
+ string scratch = "";
if (fname == "COUT" || fname == "cout") {
buffer = cout.rdbuf();
// Nothing here, yet
}
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";
+ outstream << delimeter;
+ outstream << "Aileron Cmd" + delimeter;
+ outstream << "Elevator Cmd" + delimeter;
+ outstream << "Rudder Cmd" + delimeter;
+ outstream << "Flap Cmd" + delimeter;
+ outstream << "Left Aileron Pos" + delimeter;
+ outstream << "Right Aileron Pos" + delimeter;
+ outstream << "Elevator Pos" + delimeter;
+ outstream << "Rudder Pos" + delimeter;
+ outstream << "Flap Pos";
}
if (SubSystems & ssRates) {
- outstream << ", ";
- outstream << "P, Q, R, ";
- outstream << "Pdot, Qdot, Rdot";
+ outstream << delimeter;
+ outstream << "P" + delimeter + "Q" + delimeter + "R" + delimeter;
+ outstream << "Pdot" + delimeter + "Qdot" + delimeter + "Rdot";
}
if (SubSystems & ssVelocities) {
- outstream << ", ";
- outstream << "QBar, ";
- outstream << "Vtotal, ";
- outstream << "UBody, VBody, WBody, ";
- outstream << "UAero, VAero, WAero, ";
- outstream << "Vn, Ve, Vd";
+ outstream << delimeter;
+ outstream << "QBar" + delimeter;
+ outstream << "Vtotal" + delimeter;
+ outstream << "UBody" + delimeter + "VBody" + delimeter + "WBody" + delimeter;
+ outstream << "UAero" + delimeter + "VAero" + delimeter + "WAero" + delimeter;
+ outstream << "Vn" + delimeter + "Ve" + delimeter + "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";
+ outstream << delimeter;
+ outstream << "Drag" + delimeter + "Side" + delimeter + "Lift" + delimeter;
+ outstream << "L/D" + delimeter;
+ outstream << "Xforce" + delimeter + "Yforce" + delimeter + "Zforce";
}
if (SubSystems & ssMoments) {
- outstream << ", ";
- outstream << "L, M, N";
+ outstream << delimeter;
+ outstream << "L" + delimeter + "M" + delimeter + "N";
}
if (SubSystems & ssAtmosphere) {
- outstream << ", ";
- outstream << "Rho, ";
- outstream << "NWind, EWind, DWind";
+ outstream << delimeter;
+ outstream << "Rho" + delimeter;
+ outstream << "NWind" + delimeter + "EWind" + delimeter + "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 << delimeter;
+ outstream << "Ixx" + delimeter;
+ outstream << "Ixy" + delimeter;
+ outstream << "Ixz" + delimeter;
+ outstream << "Iyx" + delimeter;
+ outstream << "Iyy" + delimeter;
+ outstream << "Iyz" + delimeter;
+ outstream << "Izx" + delimeter;
+ outstream << "Izy" + delimeter;
+ outstream << "Izz" + delimeter;
+ outstream << "Mass" + delimeter;
+ outstream << "Xcg" + delimeter + "Ycg" + delimeter + "Zcg";
+ }
+ if (SubSystems & ssPropagate) {
+ outstream << delimeter;
+ outstream << "Altitude" + delimeter;
+ outstream << "Phi" + delimeter + "Tht" + delimeter + "Psi" + delimeter;
+ outstream << "Alpha" + delimeter;
+ outstream << "Beta" + delimeter;
+ outstream << "Latitude (Deg)" + delimeter;
+ outstream << "Longitude (Deg)" + delimeter;
+ outstream << "Distance AGL" + delimeter;
outstream << "Runway Radius";
}
if (SubSystems & ssCoefficients) {
- outstream << ", ";
- outstream << Aerodynamics->GetCoefficientStrings();
+ scratch = Aerodynamics->GetCoefficientStrings(delimeter);
+ if (scratch.length() != 0) outstream << delimeter << scratch;
}
if (SubSystems & ssFCS) {
- outstream << ", ";
- outstream << FCS->GetComponentStrings();
+ scratch = FCS->GetComponentStrings(delimeter);
+ if (scratch.length() != 0) outstream << delimeter << scratch;
}
if (SubSystems & ssGroundReactions) {
- outstream << ", ";
- outstream << GroundReactions->GetGroundReactionStrings();
+ outstream << delimeter;
+ outstream << GroundReactions->GetGroundReactionStrings(delimeter);
}
if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
- outstream << ", ";
- outstream << Propulsion->GetPropulsionStrings();
+ outstream << delimeter;
+ outstream << Propulsion->GetPropulsionStrings(delimeter);
}
if (OutputProperties.size() > 0) {
- for (int i=0;i<OutputProperties.size();i++) {
- outstream << ", " << OutputProperties[i]->GetName();
+ for (unsigned int i=0;i<OutputProperties.size();i++) {
+ outstream << delimeter << OutputProperties[i]->GetName();
}
}
if (SubSystems & ssSimulation) {
}
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 << delimeter;
+ outstream << FCS->GetDaCmd() << delimeter;
+ outstream << FCS->GetDeCmd() << delimeter;
+ outstream << FCS->GetDrCmd() << delimeter;
+ outstream << FCS->GetDfCmd() << delimeter;
+ outstream << FCS->GetDaLPos() << delimeter;
+ outstream << FCS->GetDaRPos() << delimeter;
+ outstream << FCS->GetDePos() << delimeter;
+ outstream << FCS->GetDrPos() << delimeter;
outstream << FCS->GetDfPos();
}
if (SubSystems & ssRates) {
- outstream << ", ";
- outstream << Rotation->GetPQR() << ", ";
- outstream << Rotation->GetPQRdot();
+ outstream << delimeter;
+ outstream << Propagate->GetPQR().Dump(delimeter) << delimeter;
+ outstream << Propagate->GetPQRdot().Dump(delimeter);
}
if (SubSystems & ssVelocities) {
- outstream << ", ";
- outstream << Translation->Getqbar() << ", ";
- outstream << Translation->GetVt() << ", ";
- outstream << Translation->GetUVW() << ", ";
- outstream << Translation->GetAeroUVW() << ", ";
- outstream << Position->GetVel();
+ outstream << delimeter;
+ outstream << Auxiliary->Getqbar() << delimeter;
+ outstream << setprecision(12) << Auxiliary->GetVt() << delimeter;
+ outstream << setprecision(12) << Propagate->GetUVW().Dump(delimeter) << delimeter;
+ outstream << Auxiliary->GetAeroUVW().Dump(delimeter) << delimeter;
+ outstream << Propagate->GetVel().Dump(delimeter);
}
if (SubSystems & ssForces) {
- outstream << ", ";
- outstream << Aerodynamics->GetvFs() << ", ";
- outstream << Aerodynamics->GetLoD() << ", ";
- outstream << Aircraft->GetForces() << ", ";
- outstream << Inertial->GetGravity() << ", ";
- outstream << Inertial->GetCoriolis() << ", ";
- outstream << Inertial->GetCentrifugal();
+ outstream << delimeter;
+ outstream << Aerodynamics->GetvFs() << delimeter;
+ outstream << Aerodynamics->GetLoD() << delimeter;
+ outstream << Aircraft->GetForces().Dump(delimeter);
}
if (SubSystems & ssMoments) {
- outstream << ", ";
- outstream << Aircraft->GetMoments();
+ outstream << delimeter;
+ outstream << Aircraft->GetMoments().Dump(delimeter);
}
if (SubSystems & ssAtmosphere) {
- outstream << ", ";
- outstream << Atmosphere->GetDensity() << ", ";
- outstream << Atmosphere->GetWindNED();
+ outstream << delimeter;
+ outstream << Atmosphere->GetDensity() << delimeter;
+ outstream << Atmosphere->GetWindNED().Dump(delimeter);
}
if (SubSystems & ssMassProps) {
- outstream << ", ";
- outstream << MassBalance->GetIxx() << ", ";
- outstream << MassBalance->GetIyy() << ", ";
- outstream << MassBalance->GetIzz() << ", ";
- outstream << MassBalance->GetIxz() << ", ";
- outstream << MassBalance->GetMass() << ", ";
+ outstream << delimeter;
+ outstream << MassBalance->GetJ() << delimeter;
+ outstream << MassBalance->GetMass() << delimeter;
outstream << MassBalance->GetXYZcg();
}
- 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 & ssPropagate) {
+ outstream << delimeter;
+ outstream << Propagate->Geth() << delimeter;
+ outstream << Propagate->GetEuler().Dump(delimeter) << delimeter;
+ outstream << Auxiliary->Getalpha(inDegrees) << delimeter;
+ outstream << Auxiliary->Getbeta(inDegrees) << delimeter;
+ outstream << Propagate->GetLocation().GetLatitudeDeg() << delimeter;
+ outstream << Propagate->GetLocation().GetLongitudeDeg() << delimeter;
+ outstream << Propagate->GetDistanceAGL() << delimeter;
+ outstream << Propagate->GetRunwayRadius();
}
if (SubSystems & ssCoefficients) {
- outstream << ", ";
- outstream << Aerodynamics->GetCoefficientValues();
+ scratch = Aerodynamics->GetCoefficientValues(delimeter);
+ if (scratch.length() != 0) outstream << delimeter << scratch;
}
if (SubSystems & ssFCS) {
- outstream << ", ";
- outstream << FCS->GetComponentValues();
+ scratch = FCS->GetComponentValues(delimeter);
+ if (scratch.length() != 0) outstream << delimeter << scratch;
}
if (SubSystems & ssGroundReactions) {
- outstream << ", ";
- outstream << GroundReactions->GetGroundReactionValues();
+ outstream << delimeter;
+ outstream << GroundReactions->GetGroundReactionValues(delimeter);
}
if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
- outstream << ", ";
- outstream << Propulsion->GetPropulsionValues();
+ outstream << delimeter;
+ outstream << Propulsion->GetPropulsionValues(delimeter);
}
- for (int i=0;i<OutputProperties.size();i++) {
- outstream << ", " << OutputProperties[i]->getDoubleValue();
+ for (unsigned int i=0;i<OutputProperties.size();i++) {
+ outstream << delimeter << OutputProperties[i]->getDoubleValue();
}
outstream << endl;
socket->Append("Fx");
socket->Append("Fy");
socket->Append("Fz");
- socket->Append("Latitude");
- socket->Append("Longitude");
+ socket->Append("Latitude (Deg)");
+ socket->Append("Longitude (Deg)");
socket->Append("QBar");
socket->Append("Alpha");
socket->Append("L");
socket->Clear();
socket->Append(State->Getsim_time());
- socket->Append(Position->Geth());
- socket->Append(Rotation->Getphi());
- socket->Append(Rotation->Gettht());
- socket->Append(Rotation->Getpsi());
+ socket->Append(Propagate->Geth());
+ socket->Append(Propagate->GetEuler(ePhi));
+ socket->Append(Propagate->GetEuler(eTht));
+ socket->Append(Propagate->GetEuler(ePsi));
socket->Append(Atmosphere->GetDensity());
- socket->Append(Translation->GetVt());
- socket->Append(Translation->GetUVW(eU));
- socket->Append(Translation->GetUVW(eV));
- socket->Append(Translation->GetUVW(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->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(Auxiliary->GetVt());
+ socket->Append(Propagate->GetUVW(eU));
+ socket->Append(Propagate->GetUVW(eV));
+ socket->Append(Propagate->GetUVW(eW));
+ socket->Append(Auxiliary->GetAeroUVW(eU));
+ socket->Append(Auxiliary->GetAeroUVW(eV));
+ socket->Append(Auxiliary->GetAeroUVW(eW));
+ socket->Append(Propagate->GetVel(eNorth));
+ socket->Append(Propagate->GetVel(eEast));
+ socket->Append(Propagate->GetVel(eDown));
+ socket->Append(Propagate->GetUVWdot(eU));
+ socket->Append(Propagate->GetUVWdot(eV));
+ socket->Append(Propagate->GetUVWdot(eW));
+ socket->Append(Propagate->GetPQR(eP));
+ socket->Append(Propagate->GetPQR(eQ));
+ socket->Append(Propagate->GetPQR(eR));
+ socket->Append(Propagate->GetPQRdot(eP));
+ socket->Append(Propagate->GetPQRdot(eQ));
+ socket->Append(Propagate->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(Propagate->GetLocation().GetLatitudeDeg());
+ socket->Append(Propagate->GetLocation().GetLongitudeDeg());
+ socket->Append(Auxiliary->Getqbar());
+ socket->Append(Auxiliary->Getalpha(inDegrees));
socket->Append(Aircraft->GetMoments(eL));
socket->Append(Aircraft->GetMoments(eM));
socket->Append(Aircraft->GetMoments(eN));
int OutRate = 0;
FGConfigFile* Output_cfg;
string property;
+ unsigned int port;
# ifndef macintosh
separator = "/";
name = AC_cfg->GetValue("NAME");
fname = AC_cfg->GetValue("FILE");
token = AC_cfg->GetValue("TYPE");
+ port = atoi(AC_cfg->GetValue("PORT").c_str());
+
Output->SetType(token);
-#if defined( FG_WITH_JSBSIM_SOCKET ) || !defined( FGFS )
if (token == "SOCKET") {
- socket = new FGfdmSocket("localhost",1138);
+ socket = new FGfdmSocket(name,port);
}
-#endif
if (!fname.empty()) {
outputInFileName = FDMExec->GetAircraftPath() + separator
}
if (parameter == "POSITION") {
*Output_cfg >> parameter;
- if (parameter == "ON") SubSystems += ssPosition;
+ if (parameter == "ON") SubSystems += ssPropagate;
}
if (parameter == "COEFFICIENTS") {
*Output_cfg >> parameter;
OutputProperties.push_back(PropertyManager->GetNode(property));
}
- if (Output_cfg->GetNextConfigLine() == "EOF") break;
+ if (parameter == "EOF") break;
}
OutRate = OutRate>120?120:(OutRate<0?0:OutRate);
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()) {
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 & ssPropagate) cout << " Propagate 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 (OutputProperties.size() > 0) cout << " Properties logged:" << endl;
+ for (unsigned int i=0;i<OutputProperties.size();i++) {
+ cout << " - " << OutputProperties[i]->GetName() << endl;
+ }
}
}
if (debug_lvl & 2 ) { // Instantiation/Destruction notification
projects / flightgear.git / blobdiff