-/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%\r
-\r
- Module: FGOutput.cpp\r
- Author: Jon Berndt\r
- Date started: 12/02/98\r
- Purpose: Manage output of sim parameters to file or stdout\r
- Called by: FGSimExec\r
-\r
- ------------- Copyright (C) 1999 Jon S. Berndt (jsb@hal-pc.org) -------------\r
-\r
- This program is free software; you can redistribute it and/or modify it under\r
- the terms of the GNU General Public License as published by the Free Software\r
- Foundation; either version 2 of the License, or (at your option) any later\r
- version.\r
-\r
- This program is distributed in the hope that it will be useful, but WITHOUT\r
- ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS\r
- FOR A PARTICULAR PURPOSE. See the GNU General Public License for more\r
- details.\r
-\r
- You should have received a copy of the GNU General Public License along with\r
- this program; if not, write to the Free Software Foundation, Inc., 59 Temple\r
- Place - Suite 330, Boston, MA 02111-1307, USA.\r
-\r
- Further information about the GNU General Public License can also be found on\r
- the world wide web at http://www.gnu.org.\r
-\r
-FUNCTIONAL DESCRIPTION\r
---------------------------------------------------------------------------------\r
-This is the place where you create output routines to dump data for perusal\r
-later.\r
-\r
-HISTORY\r
---------------------------------------------------------------------------------\r
-12/02/98 JSB Created\r
-\r
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%\r
-INCLUDES\r
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/\r
-\r
-#include "FGOutput.h"\r
-#include "FGState.h"\r
-#include "FGFDMExec.h"\r
-#include "FGAtmosphere.h"\r
-#include "FGFCS.h"\r
-#include "FGAerodynamics.h"\r
-#include "FGGroundReactions.h"\r
-#include "FGAircraft.h"\r
-#include "FGMassBalance.h"\r
-#include "FGTranslation.h"\r
-#include "FGRotation.h"\r
-#include "FGPosition.h"\r
-#include "FGAuxiliary.h"\r
-#include "FGInertial.h"\r
-\r
-namespace JSBSim {\r
-\r
-static const char *IdSrc = "$Id$";\r
-static const char *IdHdr = ID_OUTPUT;\r
-\r
-/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%\r
-CLASS IMPLEMENTATION\r
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/\r
-\r
-FGOutput::FGOutput(FGFDMExec* fdmex) : FGModel(fdmex)\r
-{\r
- Name = "FGOutput";\r
- sFirstPass = dFirstPass = true;\r
- socket = 0;\r
- Type = otNone;\r
- Filename = "";\r
- SubSystems = 0;\r
- enabled = true;\r
- outputInFileName = "";\r
-\r
- Debug(0);\r
-}\r
-\r
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%\r
-\r
-FGOutput::~FGOutput()\r
-{\r
- if (socket) delete socket;\r
- for (unsigned int i=0; i<OutputProperties.size(); i++) delete OutputProperties[i];\r
-\r
- Debug(1);\r
-}\r
-\r
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%\r
-\r
-bool FGOutput::Run(void)\r
-{\r
- if (enabled) {\r
- if (!FGModel::Run()) {\r
-\r
- if (Type == otSocket) {\r
- SocketOutput();\r
- } else if (Type == otCSV) {\r
- DelimitedOutput(Filename);\r
- } else if (Type == otTerminal) {\r
- // Not done yet\r
- } else if (Type == otNone) {\r
- // Do nothing\r
- } else {\r
- // Not a valid type of output\r
- }\r
- return false;\r
- } else {\r
- return true;\r
- }\r
- }\r
- return false;\r
-}\r
-\r
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%\r
-\r
-void FGOutput::SetType(string type)\r
-{\r
- if (type == "CSV") {\r
- Type = otCSV;\r
- } else if (type == "TABULAR") {\r
- Type = otTab;\r
- } else if (type == "SOCKET") {\r
- Type = otSocket;\r
- } else if (type == "TERMINAL") {\r
- Type = otTerminal;\r
- } else if (type != string("NONE")) {\r
- Type = otUnknown;\r
- cerr << "Unknown type of output specified in config file" << endl;\r
- }\r
-}\r
-\r
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%\r
-\r
-void FGOutput::DelimitedOutput(string fname)\r
-{\r
- streambuf* buffer;\r
- string scratch = "";\r
-\r
- if (fname == "COUT" || fname == "cout") {\r
- buffer = cout.rdbuf();\r
- } else {\r
- datafile.open(fname.c_str());\r
- buffer = datafile.rdbuf();\r
- }\r
-\r
- ostream outstream(buffer);\r
-\r
- if (dFirstPass) {\r
- outstream << "Time";\r
- if (SubSystems & ssSimulation) {\r
- // Nothing here, yet\r
- }\r
- if (SubSystems & ssAerosurfaces) {\r
- outstream << ", ";\r
- outstream << "Aileron Cmd, ";\r
- outstream << "Elevator Cmd, ";\r
- outstream << "Rudder Cmd, ";\r
- outstream << "Flap Cmd, ";\r
- outstream << "Left Aileron Pos, ";\r
- outstream << "Right Aileron Pos, ";\r
- outstream << "Elevator Pos, ";\r
- outstream << "Rudder Pos, ";\r
- outstream << "Flap Pos";\r
- }\r
- if (SubSystems & ssRates) {\r
- outstream << ", ";\r
- outstream << "P, Q, R, ";\r
- outstream << "Pdot, Qdot, Rdot";\r
- }\r
- if (SubSystems & ssVelocities) {\r
- outstream << ", ";\r
- outstream << "QBar, ";\r
- outstream << "Vtotal, ";\r
- outstream << "UBody, VBody, WBody, ";\r
- outstream << "UAero, VAero, WAero, ";\r
- outstream << "Vn, Ve, Vd";\r
- }\r
- if (SubSystems & ssForces) {\r
- outstream << ", ";\r
- outstream << "Drag, Side, Lift, ";\r
- outstream << "L/D, ";\r
- outstream << "Xforce, Yforce, Zforce, ";\r
- outstream << "xGravity, yGravity, zGravity, ";\r
- outstream << "xCoriolis, yCoriolis, zCoriolis, ";\r
- outstream << "xCentrifugal, yCentrifugal, zCentrifugal";\r
- }\r
- if (SubSystems & ssMoments) {\r
- outstream << ", ";\r
- outstream << "L, M, N";\r
- }\r
- if (SubSystems & ssAtmosphere) {\r
- outstream << ", ";\r
- outstream << "Rho, ";\r
- outstream << "NWind, EWind, DWind";\r
- }\r
- if (SubSystems & ssMassProps) {\r
- outstream << ", ";\r
- outstream << "Ixx, ";\r
- outstream << "Ixy, ";\r
- outstream << "Ixz, ";\r
- outstream << "Iyx, ";\r
- outstream << "Iyy, ";\r
- outstream << "Iyz, ";\r
- outstream << "Izx, ";\r
- outstream << "Izy, ";\r
- outstream << "Izz, ";\r
- outstream << "Mass, ";\r
- outstream << "Xcg, Ycg, Zcg";\r
- }\r
- if (SubSystems & ssPosition) {\r
- outstream << ", ";\r
- outstream << "Altitude, ";\r
- outstream << "Phi, Tht, Psi, ";\r
- outstream << "Alpha, ";\r
- outstream << "Beta, ";\r
- outstream << "Latitude, ";\r
- outstream << "Longitude, ";\r
- outstream << "Distance AGL, ";\r
- outstream << "Runway Radius";\r
- }\r
- if (SubSystems & ssCoefficients) {\r
- scratch = Aerodynamics->GetCoefficientStrings();\r
- if (scratch.length() != 0) outstream << ", " << scratch;\r
- }\r
- if (SubSystems & ssFCS) {\r
- scratch = FCS->GetComponentStrings();\r
- if (scratch.length() != 0) outstream << ", " << scratch;\r
- }\r
- if (SubSystems & ssGroundReactions) {\r
- outstream << ", ";\r
- outstream << GroundReactions->GetGroundReactionStrings();\r
- }\r
- if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {\r
- outstream << ", ";\r
- outstream << Propulsion->GetPropulsionStrings();\r
- }\r
- if (OutputProperties.size() > 0) {\r
- for (unsigned int i=0;i<OutputProperties.size();i++) {\r
- outstream << ", " << OutputProperties[i]->GetName();\r
- }\r
- }\r
-\r
- outstream << endl;\r
- dFirstPass = false;\r
- }\r
-\r
- outstream << State->Getsim_time();\r
- if (SubSystems & ssSimulation) {\r
- }\r
- if (SubSystems & ssAerosurfaces) {\r
- outstream << ", ";\r
- outstream << FCS->GetDaCmd() << ", ";\r
- outstream << FCS->GetDeCmd() << ", ";\r
- outstream << FCS->GetDrCmd() << ", ";\r
- outstream << FCS->GetDfCmd() << ", ";\r
- outstream << FCS->GetDaLPos() << ", ";\r
- outstream << FCS->GetDaRPos() << ", ";\r
- outstream << FCS->GetDePos() << ", ";\r
- outstream << FCS->GetDrPos() << ", ";\r
- outstream << FCS->GetDfPos();\r
- }\r
- if (SubSystems & ssRates) {\r
- outstream << ", ";\r
- outstream << Rotation->GetPQR() << ", ";\r
- outstream << Rotation->GetPQRdot();\r
- }\r
- if (SubSystems & ssVelocities) {\r
- outstream << ", ";\r
- outstream << Translation->Getqbar() << ", ";\r
- outstream << Translation->GetVt() << ", ";\r
- outstream << Translation->GetUVW() << ", ";\r
- outstream << Translation->GetAeroUVW() << ", ";\r
- outstream << Position->GetVel();\r
- }\r
- if (SubSystems & ssForces) {\r
- outstream << ", ";\r
- outstream << Aerodynamics->GetvFs() << ", ";\r
- outstream << Aerodynamics->GetLoD() << ", ";\r
- outstream << Aircraft->GetForces() << ", ";\r
- outstream << Inertial->GetGravity() << ", ";\r
- outstream << Inertial->GetCoriolis() << ", ";\r
- outstream << Inertial->GetCentrifugal();\r
- }\r
- if (SubSystems & ssMoments) {\r
- outstream << ", ";\r
- outstream << Aircraft->GetMoments();\r
- }\r
- if (SubSystems & ssAtmosphere) {\r
- outstream << ", ";\r
- outstream << Atmosphere->GetDensity() << ", ";\r
- outstream << Atmosphere->GetWindNED();\r
- }\r
- if (SubSystems & ssMassProps) {\r
- outstream << ", ";\r
- outstream << MassBalance->GetJ() << ", ";\r
- outstream << MassBalance->GetMass() << ", ";\r
- outstream << MassBalance->GetXYZcg();\r
- }\r
- if (SubSystems & ssPosition) {\r
- outstream << ", ";\r
- outstream << Position->Geth() << ", ";\r
- outstream << Rotation->GetEuler() << ", ";\r
- outstream << Translation->Getalpha() << ", ";\r
- outstream << Translation->Getbeta() << ", ";\r
- outstream << Position->GetLatitude() << ", ";\r
- outstream << Position->GetLongitude() << ", ";\r
- outstream << Position->GetDistanceAGL() << ", ";\r
- outstream << Position->GetRunwayRadius();\r
- }\r
- if (SubSystems & ssCoefficients) {\r
- scratch = Aerodynamics->GetCoefficientValues();\r
- if (scratch.length() != 0) outstream << ", " << scratch;\r
- }\r
- if (SubSystems & ssFCS) {\r
- scratch = FCS->GetComponentValues();\r
- if (scratch.length() != 0) outstream << ", " << scratch;\r
- }\r
- if (SubSystems & ssGroundReactions) {\r
- outstream << ", ";\r
- outstream << GroundReactions->GetGroundReactionValues();\r
- }\r
- if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {\r
- outstream << ", ";\r
- outstream << Propulsion->GetPropulsionValues();\r
- }\r
-\r
- for (unsigned int i=0;i<OutputProperties.size();i++) {\r
- outstream << ", " << OutputProperties[i]->getDoubleValue();\r
- }\r
-\r
- outstream << endl;\r
- outstream.flush();\r
-}\r
-\r
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%\r
-\r
-void FGOutput::SocketOutput(void)\r
-{\r
- string asciiData;\r
-\r
- if (socket == NULL) return;\r
- if (!socket->GetConnectStatus()) return;\r
-\r
- socket->Clear();\r
- if (sFirstPass) {\r
- socket->Append("<LABELS>");\r
- socket->Append("Time");\r
- socket->Append("Altitude");\r
- socket->Append("Phi");\r
- socket->Append("Tht");\r
- socket->Append("Psi");\r
- socket->Append("Rho");\r
- socket->Append("Vtotal");\r
- socket->Append("UBody");\r
- socket->Append("VBody");\r
- socket->Append("WBody");\r
- socket->Append("UAero");\r
- socket->Append("VAero");\r
- socket->Append("WAero");\r
- socket->Append("Vn");\r
- socket->Append("Ve");\r
- socket->Append("Vd");\r
- socket->Append("Udot");\r
- socket->Append("Vdot");\r
- socket->Append("Wdot");\r
- socket->Append("P");\r
- socket->Append("Q");\r
- socket->Append("R");\r
- socket->Append("PDot");\r
- socket->Append("QDot");\r
- socket->Append("RDot");\r
- socket->Append("Fx");\r
- socket->Append("Fy");\r
- socket->Append("Fz");\r
- socket->Append("Latitude");\r
- socket->Append("Longitude");\r
- socket->Append("QBar");\r
- socket->Append("Alpha");\r
- socket->Append("L");\r
- socket->Append("M");\r
- socket->Append("N");\r
- socket->Append("Throttle Position");\r
- socket->Append("Left Aileron Position");\r
- socket->Append("Right Aileron Position");\r
- socket->Append("Elevator Position");\r
- socket->Append("Rudder Position");\r
- sFirstPass = false;\r
- socket->Send();\r
- }\r
-\r
- socket->Clear();\r
- socket->Append(State->Getsim_time());\r
- socket->Append(Position->Geth());\r
- socket->Append(Rotation->Getphi());\r
- socket->Append(Rotation->Gettht());\r
- socket->Append(Rotation->Getpsi());\r
- socket->Append(Atmosphere->GetDensity());\r
- socket->Append(Translation->GetVt());\r
- socket->Append(Translation->GetUVW(eU));\r
- socket->Append(Translation->GetUVW(eV));\r
- socket->Append(Translation->GetUVW(eW));\r
- socket->Append(Translation->GetAeroUVW(eU));\r
- socket->Append(Translation->GetAeroUVW(eV));\r
- socket->Append(Translation->GetAeroUVW(eW));\r
- socket->Append(Position->GetVn());\r
- socket->Append(Position->GetVe());\r
- socket->Append(Position->GetVd());\r
- socket->Append(Translation->GetUVWdot(eU));\r
- socket->Append(Translation->GetUVWdot(eV));\r
- socket->Append(Translation->GetUVWdot(eW));\r
- socket->Append(Rotation->GetPQR(eP));\r
- socket->Append(Rotation->GetPQR(eQ));\r
- socket->Append(Rotation->GetPQR(eR));\r
- socket->Append(Rotation->GetPQRdot(eP));\r
- socket->Append(Rotation->GetPQRdot(eQ));\r
- socket->Append(Rotation->GetPQRdot(eR));\r
- socket->Append(Aircraft->GetForces(eX));\r
- socket->Append(Aircraft->GetForces(eY));\r
- socket->Append(Aircraft->GetForces(eZ));\r
- socket->Append(Position->GetLatitude());\r
- socket->Append(Position->GetLongitude());\r
- socket->Append(Translation->Getqbar());\r
- socket->Append(Translation->Getalpha());\r
- socket->Append(Aircraft->GetMoments(eL));\r
- socket->Append(Aircraft->GetMoments(eM));\r
- socket->Append(Aircraft->GetMoments(eN));\r
- socket->Append(FCS->GetThrottlePos(0));\r
- socket->Append(FCS->GetDaLPos());\r
- socket->Append(FCS->GetDaRPos());\r
- socket->Append(FCS->GetDePos());\r
- socket->Append(FCS->GetDrPos());\r
- socket->Send();\r
-}\r
-\r
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%\r
-\r
-void FGOutput::SocketStatusOutput(string out_str)\r
-{\r
- string asciiData;\r
-\r
- if (socket == NULL) return;\r
-\r
- socket->Clear();\r
- asciiData = string("<STATUS>") + out_str;\r
- socket->Append(asciiData.c_str());\r
- socket->Send();\r
-}\r
-\r
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%\r
-\r
-bool FGOutput::Load(FGConfigFile* AC_cfg)\r
-{\r
- string token="", parameter="", separator="";\r
- string name="", fname="";\r
- int OutRate = 0;\r
- FGConfigFile* Output_cfg;\r
- string property;\r
-\r
-# ifndef macintosh\r
- separator = "/";\r
-# else\r
- separator = ";";\r
-# endif\r
-\r
- name = AC_cfg->GetValue("NAME");\r
- fname = AC_cfg->GetValue("FILE");\r
- token = AC_cfg->GetValue("TYPE");\r
- Output->SetType(token);\r
-\r
-#if defined( FG_WITH_JSBSIM_SOCKET ) || !defined( FGFS )\r
- if (token == "SOCKET") {\r
- socket = new FGfdmSocket("localhost",1138);\r
- }\r
-#endif\r
-\r
- if (!fname.empty()) {\r
- outputInFileName = FDMExec->GetAircraftPath() + separator\r
- + FDMExec->GetModelName() + separator + fname + ".xml";\r
- Output_cfg = new FGConfigFile(outputInFileName);\r
- if (!Output_cfg->IsOpen()) {\r
- cerr << "Could not open file: " << outputInFileName << endl;\r
- return false;\r
- }\r
- } else {\r
- Output_cfg = AC_cfg;\r
- }\r
- Output->SetFilename(name);\r
-\r
- while ((token = Output_cfg->GetValue()) != string("/OUTPUT")) {\r
- *Output_cfg >> parameter;\r
- if (parameter == "RATE_IN_HZ") {\r
- *Output_cfg >> OutRate;\r
- }\r
- if (parameter == "SIMULATION") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssSimulation;\r
- }\r
- if (parameter == "AEROSURFACES") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssAerosurfaces;\r
- }\r
- if (parameter == "RATES") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssRates;\r
- }\r
- if (parameter == "VELOCITIES") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssVelocities;\r
- }\r
- if (parameter == "FORCES") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssForces;\r
- }\r
- if (parameter == "MOMENTS") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssMoments;\r
- }\r
- if (parameter == "ATMOSPHERE") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssAtmosphere;\r
- }\r
- if (parameter == "MASSPROPS") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssMassProps;\r
- }\r
- if (parameter == "POSITION") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssPosition;\r
- }\r
- if (parameter == "COEFFICIENTS") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssCoefficients;\r
- }\r
- if (parameter == "GROUND_REACTIONS") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssGroundReactions;\r
- }\r
- if (parameter == "FCS") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssFCS;\r
- }\r
- if (parameter == "PROPULSION") {\r
- *Output_cfg >> parameter;\r
- if (parameter == "ON") SubSystems += ssPropulsion;\r
- }\r
- if (parameter == "PROPERTY") {\r
- *Output_cfg >> property;\r
- OutputProperties.push_back(PropertyManager->GetNode(property));\r
- }\r
-\r
- if (parameter == "EOF") break;\r
- }\r
-\r
- OutRate = OutRate>120?120:(OutRate<0?0:OutRate);\r
- rate = (int)(0.5 + 1.0/(State->Getdt()*OutRate));\r
-\r
- Debug(2);\r
-\r
- return true;\r
-}\r
-\r
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%\r
-// The bitmasked value choices are as follows:\r
-// unset: In this case (the default) JSBSim would only print\r
-// out the normally expected messages, essentially echoing\r
-// the config files as they are read. If the environment\r
-// variable is not set, debug_lvl is set to 1 internally\r
-// 0: This requests JSBSim not to output any messages\r
-// whatsoever.\r
-// 1: This value explicity requests the normal JSBSim\r
-// startup messages\r
-// 2: This value asks for a message to be printed out when\r
-// a class is instantiated\r
-// 4: When this value is set, a message is displayed when a\r
-// FGModel object executes its Run() method\r
-// 8: When this value is set, various runtime state variables\r
-// are printed out periodically\r
-// 16: When set various parameters are sanity checked and\r
-// a message is printed out when they go out of bounds\r
-\r
-void FGOutput::Debug(int from)\r
-{\r
- string scratch="";\r
-\r
- if (debug_lvl <= 0) return;\r
-\r
- if (debug_lvl & 1) { // Standard console startup message output\r
- if (from == 0) { // Constructor\r
-\r
- }\r
- if (from == 2) {\r
- if (outputInFileName.empty())\r
- cout << " " << "Output parameters read inline" << endl;\r
- else\r
- cout << " Output parameters read from file: " << outputInFileName << endl;\r
-\r
- if (Filename == "cout" || Filename == "COUT") {\r
- scratch = " Log output goes to screen console";\r
- } else if (!Filename.empty()) {\r
- scratch = " Log output goes to file: " + Filename;\r
- }\r
- switch (Type) {\r
- case otCSV:\r
- cout << scratch << " in CSV format output at rate " << 120/rate << " Hz" << endl;\r
- break;\r
- case otNone:\r
- cout << " No log output" << endl;\r
- break;\r
- }\r
-\r
- if (SubSystems & ssSimulation) cout << " Simulation parameters logged" << endl;\r
- if (SubSystems & ssAerosurfaces) cout << " Aerosurface parameters logged" << endl;\r
- if (SubSystems & ssRates) cout << " Rate parameters logged" << endl;\r
- if (SubSystems & ssVelocities) cout << " Velocity parameters logged" << endl;\r
- if (SubSystems & ssForces) cout << " Force parameters logged" << endl;\r
- if (SubSystems & ssMoments) cout << " Moments parameters logged" << endl;\r
- if (SubSystems & ssAtmosphere) cout << " Atmosphere parameters logged" << endl;\r
- if (SubSystems & ssMassProps) cout << " Mass parameters logged" << endl;\r
- if (SubSystems & ssCoefficients) cout << " Coefficient parameters logged" << endl;\r
- if (SubSystems & ssPosition) cout << " Position parameters logged" << endl;\r
- if (SubSystems & ssGroundReactions) cout << " Ground parameters logged" << endl;\r
- if (SubSystems & ssFCS) cout << " FCS parameters logged" << endl;\r
- if (SubSystems & ssPropulsion) cout << " Propulsion parameters logged" << endl;\r
- }\r
- }\r
- if (debug_lvl & 2 ) { // Instantiation/Destruction notification\r
- if (from == 0) cout << "Instantiated: FGOutput" << endl;\r
- if (from == 1) cout << "Destroyed: FGOutput" << endl;\r
- }\r
- if (debug_lvl & 4 ) { // Run() method entry print for FGModel-derived objects\r
- }\r
- if (debug_lvl & 8 ) { // Runtime state variables\r
- }\r
- if (debug_lvl & 16) { // Sanity checking\r
- }\r
- if (debug_lvl & 64) {\r
- if (from == 0) { // Constructor\r
- cout << IdSrc << endl;\r
- cout << IdHdr << endl;\r
- }\r
- }\r
-}\r
-}\r
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+ Module: FGOutput.cpp
+ Author: Jon Berndt
+ Date started: 12/02/98
+ Purpose: Manage output of sim parameters to file or stdout
+ Called by: FGSimExec
+
+ ------------- Copyright (C) 1999 Jon S. Berndt (jsb@hal-pc.org) -------------
+
+ This program is free software; you can redistribute it and/or modify it under
+ the terms of the GNU General Public License as published by the Free Software
+ Foundation; either version 2 of the License, or (at your option) any later
+ version.
+
+ This program is distributed in the hope that it will be useful, but WITHOUT
+ ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
+ FOR A PARTICULAR PURPOSE. See the GNU General Public License for more
+ details.
+
+ You should have received a copy of the GNU General Public License along with
+ this program; if not, write to the Free Software Foundation, Inc., 59 Temple
+ Place - Suite 330, Boston, MA 02111-1307, USA.
+
+ Further information about the GNU General Public License can also be found on
+ the world wide web at http://www.gnu.org.
+
+FUNCTIONAL DESCRIPTION
+--------------------------------------------------------------------------------
+This is the place where you create output routines to dump data for perusal
+later.
+
+HISTORY
+--------------------------------------------------------------------------------
+12/02/98 JSB Created
+
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+INCLUDES
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
+
+#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 "FGMassBalance.h"
+#include "FGPropagate.h"
+#include "FGAuxiliary.h"
+#include "FGInertial.h"
+
+#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";
+ sFirstPass = dFirstPass = true;
+ socket = 0;
+ Type = otNone;
+ Filename = "";
+ SubSystems = 0;
+ enabled = true;
+ outputInFileName = "";
+ delimeter = ", ";
+
+ Debug(0);
+}
+
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+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 (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::SetType(string type)
+{
+ 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;
+ }
+}
+
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+void FGOutput::DelimitedOutput(string fname)
+{
+ streambuf* buffer;
+ string scratch = "";
+
+ if (fname == "COUT" || fname == "cout") {
+ buffer = cout.rdbuf();
+ } else {
+ datafile.open(fname.c_str());
+ buffer = datafile.rdbuf();
+ }
+
+ 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;
+ }
+
+ 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);
+ }
+
+ for (unsigned int i=0;i<OutputProperties.size();i++) {
+ outstream << delimeter << 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("<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();
+ }
+
+ 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();
+}
+
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+void FGOutput::SocketStatusOutput(string out_str)
+{
+ string asciiData;
+
+ if (socket == NULL) return;
+
+ socket->Clear();
+ asciiData = string("<STATUS>") + out_str;
+ socket->Append(asciiData.c_str());
+ socket->Send();
+}
+
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+bool FGOutput::Load(FGConfigFile* AC_cfg)
+{
+ 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 {
+ 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