-/*******************************************************************************
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
Module: FGOutput.cpp
Author: Jon Berndt
FUNCTIONAL DESCRIPTION
--------------------------------------------------------------------------------
This is the place where you create output routines to dump data for perusal
-later. Some machines may not support the ncurses console output. Borland is one
-of those environments which does not, so the ncurses stuff is commented out.
+later.
HISTORY
--------------------------------------------------------------------------------
12/02/98 JSB Created
-********************************************************************************
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
INCLUDES
-*******************************************************************************/
-
-#ifdef FGFS
-# include <Include/compiler.h>
-# ifdef FG_HAVE_STD_INCLUDES
-# include <iostream>
-# else
-# include <iostream.h>
-# endif
-#else
-# include <iostream>
-#endif
-
-#ifdef HAVE_CURSES
- #include <ncurses.h>
-#endif
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#include "FGOutput.h"
#include "FGState.h"
#include "FGFDMExec.h"
#include "FGAtmosphere.h"
#include "FGFCS.h"
+#include "FGAerodynamics.h"
+#include "FGGroundReactions.h"
#include "FGAircraft.h"
-#include "FGTranslation.h"
-#include "FGRotation.h"
-#include "FGPosition.h"
+#include "FGMassBalance.h"
+#include "FGPropagate.h"
#include "FGAuxiliary.h"
+#include "FGInertial.h"
-/*******************************************************************************
-************************************ CODE **************************************
-*******************************************************************************/
+#include <iomanip>
+
+namespace JSBSim {
+
+static const char *IdSrc = "$Id$";
+static const char *IdHdr = ID_OUTPUT;
+
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+CLASS IMPLEMENTATION
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
FGOutput::FGOutput(FGFDMExec* fdmex) : FGModel(fdmex)
{
Name = "FGOutput";
- FirstPass = true;
-#ifdef HAVE_CURSES
- initscr();
- cbreak();
- noecho();
-#endif
+ sFirstPass = dFirstPass = true;
+ socket = 0;
+ Type = otNone;
+ Filename = "";
+ SubSystems = 0;
+ enabled = true;
+ outputInFileName = "";
+ delimeter = ", ";
+
+ Debug(0);
}
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-FGOutput::~FGOutput(void)
+FGOutput::~FGOutput()
{
+ if (socket) delete socket;
+ for (unsigned int i=0; i<OutputProperties.size(); i++) delete OutputProperties[i];
+
+ Debug(1);
}
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
bool FGOutput::Run(void)
{
- if (!FGModel::Run()) {
- DelimitedOutput();
-// ConsoleOutput();
- } else {
+ if (enabled) {
+ 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 {
+ // Not a valid type of output
+ }
}
return false;
}
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGOutput::ConsoleOutput(void)
+void FGOutput::SetType(string type)
{
-#ifdef HAVE_CURSES
- string buffer;
-
- clear();
- move(1,1); insstr("Quaternions");
- move(2,5); insstr("Q0");
- move(2,16); insstr("Q1");
- move(2,27); insstr("Q2");
- move(2,38); insstr("Q3");
+ if (type == "CSV") {
+ Type = otCSV;
+ delimeter = ", ";
+ } else if (type == "TABULAR") {
+ Type = otTab;
+ delimeter = "\t";
+ } else if (type == "SOCKET") {
+ Type = otSocket;
+ } else if (type == "TERMINAL") {
+ Type = otTerminal;
+ } else if (type != string("NONE")) {
+ Type = otUnknown;
+ cerr << "Unknown type of output specified in config file" << endl;
+ }
+}
- move(3,1); buffer = Rotation->GetQ0(); insstr(buffer.c_str());
- move(3,12); buffer = Rotation->GetQ1(); insstr(buffer.c_str());
- move(3,23); buffer = Rotation->GetQ2(); insstr(buffer.c_str());
- move(3,34); buffer = Rotation->GetQ3(); insstr(buffer.c_str());
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
- move(0,0); insstr("Time: ");
- move(0,6); insstr(gcvt(State->Getsim_time(),6,buffer));
+void FGOutput::DelimitedOutput(string fname)
+{
+ streambuf* buffer;
+ string scratch = "";
- move(2,46); insstr("Phi");
- move(2,55); insstr("Tht");
- move(2,64); insstr("Psi");
+ if (fname == "COUT" || fname == "cout") {
+ buffer = cout.rdbuf();
+ } else {
+ datafile.open(fname.c_str());
+ buffer = datafile.rdbuf();
+ }
- move(3,45); buffer = Rotation->Getphi(); insstr(buffer.c_str());
- move(3,54); buffer = Rotation->Gettht(); insstr(buffer.c_str());
- move(3,63); buffer = Rotation->Getpsi(); insstr(buffer.c_str());
+ ostream outstream(buffer);
+
+ if (dFirstPass) {
+ outstream << "Time";
+ if (SubSystems & ssSimulation) {
+ // Nothing here, yet
+ }
+ if (SubSystems & ssAerosurfaces) {
+ 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 << delimeter;
+ outstream << "P" + delimeter + "Q" + delimeter + "R" + delimeter;
+ outstream << "Pdot" + delimeter + "Qdot" + delimeter + "Rdot";
+ }
+ if (SubSystems & ssVelocities) {
+ 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 << delimeter;
+ outstream << "Drag" + delimeter + "Side" + delimeter + "Lift" + delimeter;
+ outstream << "L/D" + delimeter;
+ outstream << "Xforce" + delimeter + "Yforce" + delimeter + "Zforce";
+ }
+ if (SubSystems & ssMoments) {
+ outstream << delimeter;
+ outstream << "L" + delimeter + "M" + delimeter + "N";
+ }
+ if (SubSystems & ssAtmosphere) {
+ outstream << delimeter;
+ outstream << "Rho" + delimeter;
+ outstream << "NWind" + delimeter + "EWind" + delimeter + "DWind";
+ }
+ if (SubSystems & ssMassProps) {
+ 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) {
+ scratch = Aerodynamics->GetCoefficientStrings(delimeter);
+ if (scratch.length() != 0) outstream << delimeter << scratch;
+ }
+ if (SubSystems & ssFCS) {
+ scratch = FCS->GetComponentStrings(delimeter);
+ if (scratch.length() != 0) outstream << delimeter << scratch;
+ }
+ if (SubSystems & ssGroundReactions) {
+ outstream << delimeter;
+ outstream << GroundReactions->GetGroundReactionStrings(delimeter);
+ }
+ if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
+ outstream << delimeter;
+ outstream << Propulsion->GetPropulsionStrings(delimeter);
+ }
+ if (OutputProperties.size() > 0) {
+ for (unsigned int i=0;i<OutputProperties.size();i++) {
+ outstream << delimeter << OutputProperties[i]->GetName();
+ }
+ }
+
+ outstream << endl;
+ dFirstPass = false;
+ }
- move(5,47); insstr("U");
- move(5,56); insstr("V");
- move(5,65); insstr("W");
+ outstream << State->Getsim_time();
+ if (SubSystems & ssSimulation) {
+ }
+ if (SubSystems & ssAerosurfaces) {
+ 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 << delimeter;
+ outstream << Propagate->GetPQR().Dump(delimeter) << delimeter;
+ outstream << Propagate->GetPQRdot().Dump(delimeter);
+ }
+ if (SubSystems & ssVelocities) {
+ 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 << delimeter;
+ outstream << Aerodynamics->GetvFs() << delimeter;
+ outstream << Aerodynamics->GetLoD() << delimeter;
+ outstream << Aircraft->GetForces().Dump(delimeter);
+ }
+ if (SubSystems & ssMoments) {
+ outstream << delimeter;
+ outstream << Aircraft->GetMoments().Dump(delimeter);
+ }
+ if (SubSystems & ssAtmosphere) {
+ outstream << delimeter;
+ outstream << Atmosphere->GetDensity() << delimeter;
+ outstream << Atmosphere->GetWindNED().Dump(delimeter);
+ }
+ if (SubSystems & ssMassProps) {
+ outstream << delimeter;
+ outstream << MassBalance->GetJ() << delimeter;
+ outstream << MassBalance->GetMass() << delimeter;
+ outstream << MassBalance->GetXYZcg();
+ }
+ 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) {
+ scratch = Aerodynamics->GetCoefficientValues(delimeter);
+ if (scratch.length() != 0) outstream << delimeter << scratch;
+ }
+ if (SubSystems & ssFCS) {
+ scratch = FCS->GetComponentValues(delimeter);
+ if (scratch.length() != 0) outstream << delimeter << scratch;
+ }
+ if (SubSystems & ssGroundReactions) {
+ outstream << delimeter;
+ outstream << GroundReactions->GetGroundReactionValues(delimeter);
+ }
+ if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
+ outstream << delimeter;
+ outstream << Propulsion->GetPropulsionValues(delimeter);
+ }
- move(6,45); buffer = Translation->GetU(); insstr(buffer.c_str());
- move(6,54); buffer = Translation->GetV(); insstr(buffer.c_str());
- move(6,63); buffer = Translation->GetW(); insstr(buffer.c_str());
+ for (unsigned int i=0;i<OutputProperties.size();i++) {
+ outstream << delimeter << OutputProperties[i]->getDoubleValue();
+ }
- move(8,47); insstr("Fx");
- move(8,56); insstr("Fy");
- move(8,65); insstr("Fz");
+ outstream << endl;
+ outstream.flush();
+}
- move(9,45); buffer = Aircraft->GetFx(); insstr(buffer.c_str());
- move(9,54); buffer = Aircraft->GetFy(); insstr(buffer.c_str());
- move(9,63); buffer = Aircraft->GetFz(); insstr(buffer.c_str());
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
- move(11,47); insstr("Fn");
- move(11,56); insstr("Fe");
- move(11,65); insstr("Fd");
+void FGOutput::SocketOutput(void)
+{
+ string asciiData;
+
+ if (socket == NULL) return;
+ if (!socket->GetConnectStatus()) return;
+
+ socket->Clear();
+ if (sFirstPass) {
+ socket->Append("<LABELS>");
+ socket->Append("Time");
+ socket->Append("Altitude");
+ socket->Append("Phi");
+ socket->Append("Tht");
+ socket->Append("Psi");
+ socket->Append("Rho");
+ socket->Append("Vtotal");
+ socket->Append("UBody");
+ socket->Append("VBody");
+ socket->Append("WBody");
+ socket->Append("UAero");
+ socket->Append("VAero");
+ socket->Append("WAero");
+ socket->Append("Vn");
+ socket->Append("Ve");
+ socket->Append("Vd");
+ socket->Append("Udot");
+ socket->Append("Vdot");
+ socket->Append("Wdot");
+ socket->Append("P");
+ socket->Append("Q");
+ socket->Append("R");
+ socket->Append("PDot");
+ socket->Append("QDot");
+ socket->Append("RDot");
+ socket->Append("Fx");
+ socket->Append("Fy");
+ socket->Append("Fz");
+ socket->Append("Latitude (Deg)");
+ socket->Append("Longitude (Deg)");
+ socket->Append("QBar");
+ socket->Append("Alpha");
+ socket->Append("L");
+ socket->Append("M");
+ socket->Append("N");
+ 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();
+ }
- move(12,45); buffer = Position->GetFn(); insstr(buffer.c_str());
- move(12,54); buffer = Position->GetFe(); insstr(buffer.c_str());
- move(12,63); buffer = Position->GetFd(); insstr(buffer.c_str());
+ socket->Clear();
+ socket->Append(State->Getsim_time());
+ 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(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(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));
+ socket->Append(FCS->GetThrottlePos(0));
+ socket->Append(FCS->GetDaLPos());
+ socket->Append(FCS->GetDaRPos());
+ socket->Append(FCS->GetDePos());
+ socket->Append(FCS->GetDrPos());
+ socket->Send();
+}
- move(14,47); insstr("Latitude");
- move(14,57); insstr("Longitude");
- move(14,67); insstr("Altitude");
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
- move(15,47); buffer = State->Getlatitude(); insstr(buffer.c_str());
- move(15,57); buffer = State->Getlongitude(); insstr(buffer.c_str());
- move(15,67); buffer = State->Geth(); insstr(buffer.c_str());
+void FGOutput::SocketStatusOutput(string out_str)
+{
+ string asciiData;
- refresh();
+ if (socket == NULL) return;
- move(LINES-1,1);
- refresh();
-#endif
+ socket->Clear();
+ asciiData = string("<STATUS>") + out_str;
+ socket->Append(asciiData.c_str());
+ socket->Send();
}
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGOutput::DelimitedOutput(void)
+bool FGOutput::Load(FGConfigFile* AC_cfg)
{
- if (FirstPass) {
- cout << "Time,";
- cout << "Altitude,";
- cout << "Phi,";
- cout << "Tht,";
- cout << "Psi,";
- cout << "Rho,";
- cout << "Vtotal,";
- cout << "U,";
- cout << "V,";
- cout << "W,";
- cout << "Vn,";
- cout << "Ve,";
- cout << "Vd,";
- cout << "Udot,";
- cout << "Vdot,";
- cout << "Wdot,";
- cout << "Fx,";
- cout << "Fy,";
- cout << "Fz,";
- cout << "Latitude,";
- cout << "Longitude,";
- cout << "QBar,";
- cout << "Alpha";
- cout << "L";
- cout << "M";
- cout << "N";
- cout << endl;
- FirstPass = false;
+ string token="", parameter="", separator="";
+ string name="", fname="";
+ int OutRate = 0;
+ FGConfigFile* Output_cfg;
+ string property;
+ unsigned int port;
+
+# ifndef macintosh
+ separator = "/";
+# else
+ separator = ";";
+# endif
+
+ 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 (token == "SOCKET") {
+ socket = new FGfdmSocket(name,port);
+ }
+
+ 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 {
- cout << State->Getsim_time() << ",";
- cout << State->Geth() << ",";
- cout << Rotation->Getphi() << ",";
- cout << Rotation->Gettht() << ",";
- cout << Rotation->Getpsi() << ",";
- cout << Atmosphere->Getrho() << ",";
- cout << State->GetVt() << ",";
- cout << Translation->GetU() << ",";
- cout << Translation->GetV() << ",";
- cout << Translation->GetW() << ",";
- cout << Position->GetVn() << ",";
- cout << Position->GetVe() << ",";
- cout << Position->GetVd() << ",";
- cout << Translation->GetUdot() << ",";
- cout << Translation->GetVdot() << ",";
- cout << Translation->GetWdot() << ",";
- cout << Aircraft->GetFx() << ",";
- cout << Aircraft->GetFy() << ",";
- cout << Aircraft->GetFz() << ",";
- cout << State->Getlatitude() << ",";
- cout << State->Getlongitude() << ",";
- cout << State->Getqbar() << ",";
- cout << Translation->Getalpha() << ",";
- cout << Aircraft->GetL() << ",";
- cout << Aircraft->GetM() << ",";
- cout << Aircraft->GetN() << "";
- cout << endl;
+ 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 += ssPropagate;
+ }
+ 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 & 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
+ 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