-/*******************************************************************************
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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
-*******************************************************************************/
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#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 "FGTranslation.h"
#include "FGRotation.h"
#include "FGPosition.h"
#include "FGAuxiliary.h"
-/*******************************************************************************
-************************************ CODE **************************************
-*******************************************************************************/
+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 = "JSBSim.out";
+ SubSystems = 0;
+ enabled = true;
+
#ifdef FG_WITH_JSBSIM_SOCKET
socket = new FGfdmSocket("localhost",1138);
#endif
+ Debug(0);
}
-/******************************************************************************/
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-FGOutput::~FGOutput(void)
+FGOutput::~FGOutput()
{
if (socket) delete socket;
+ Debug(1);
}
-/******************************************************************************/
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
bool FGOutput::Run(void)
{
- if (!FGModel::Run()) {
-// SocketOutput();
-// DelimitedOutput("JSBSimData.csv");
-// DelimitedOutput();
- } else {
+ 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
+ }
+
+ } else {
+ }
}
return false;
}
-/******************************************************************************/
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGOutput::DelimitedOutput(void)
+void FGOutput::SetType(string type)
{
- if (dFirstPass) {
- cout << "Time,";
- cout << "QBar,";
- cout << "Vtotal,";
- cout << "Throttle,";
- cout << "Aileron,";
- cout << "Elevator,";
- cout << "Rudder,";
- cout << "Rho,";
- cout << "Ixx,";
- cout << "Iyy,";
- cout << "Izz,";
- cout << "Ixz,";
- cout << "Mass,";
- cout << "Xcg, Ycg, Zcg, ";
- cout << "Xforce, Yforce, Zforce,";
- cout << "L, M, N, ";
- cout << "Altitude,";
- cout << "Phi, Tht, Psi,";
- cout << "P, Q, R, ";
- cout << "U, V, W, ";
- cout << "Alpha,";
- cout << "Vn, Ve, Vd, ";
- cout << "Latitude,";
- cout << "Longitude";
- cout << endl;
- dFirstPass = false;
+ if (type == "CSV") {
+ Type = otCSV;
+ } else if (type == "TABULAR") {
+ Type = otTab;
+ } 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;
}
-
- cout << State->Getsim_time() << ",";
- cout << Translation->Getqbar() << ",";
- cout << Translation->GetVt() << ",";
- cout << FCS->GetThrottlePos(0) << ",";
- cout << FCS->GetDaPos() << ",";
- cout << FCS->GetDePos() << ",";
- cout << FCS->GetDrPos() << ",";
- cout << Atmosphere->GetDensity() << ",";
- cout << Aircraft->GetIxx() << ",";
- cout << Aircraft->GetIyy() << ",";
- cout << Aircraft->GetIzz() << ",";
- cout << Aircraft->GetIxz() << ",";
- cout << Aircraft->GetMass() << ",";
- cout << Aircraft->GetXYZcg() << ",";
- cout << Aircraft->GetForces() << ",";
- cout << Aircraft->GetMoments() << ",";
- cout << Position->Geth() << ",";
- cout << Rotation->GetEuler() << ",";
- cout << Rotation->GetPQR() << ",";
- cout << Translation->GetUVW() << ",";
- cout << Translation->Getalpha() << ",";
- cout << Position->GetVel() << ",";
- cout << Position->GetLatitude() << ",";
- cout << Position->GetLongitude();
- cout << endl;
}
-/******************************************************************************/
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGOutput::DelimitedOutput(string fname)
{
- if (sFirstPass) {
+ streambuf* buffer;
+
+ if (fname == "COUT" || fname == "cout") {
+ buffer = cout.rdbuf();
+ } else {
datafile.open(fname.c_str());
- datafile << "Time,";
- datafile << "QBar,";
- datafile << "Vtotal,";
- datafile << "Throttle,";
- datafile << "Aileron,";
- datafile << "Elevator,";
- datafile << "Rudder,";
- datafile << "Rho,";
- datafile << "Ixx,";
- datafile << "Iyy,";
- datafile << "Izz,";
- datafile << "Ixz,";
- datafile << "Mass,";
- datafile << "Xcg, Ycg, Zcg, ";
- datafile << "Xforce, Yforce, Zforce, ";
- datafile << "L, M, N, ";
- datafile << "Altitude,";
- datafile << "Phi, Tht, Psi,";
- datafile << "P, Q, R, ";
- datafile << "U, V, W, ";
- datafile << "Alpha,";
- datafile << "Vn, Ve, Vd, ";
- datafile << "Latitude,";
- datafile << "Longitude";
- datafile << endl;
- sFirstPass = false;
+ buffer = datafile.rdbuf();
+ }
+
+ ostream outstream(buffer);
+
+ if (dFirstPass) {
+ outstream << "Time";
+ if (SubSystems & ssSimulation) {
+ // Nothing here, yet
+ }
+ if (SubSystems & ssAerosurfaces) {
+ outstream << ", ";
+ outstream << "Aileron Cmd, ";
+ outstream << "Elevator Cmd, ";
+ outstream << "Rudder Cmd, ";
+ outstream << "Aileron Pos, ";
+ outstream << "Elevator Pos, ";
+ outstream << "Rudder Pos";
+ }
+ if (SubSystems & ssRates) {
+ outstream << ", ";
+ outstream << "P, Q, R, ";
+ outstream << "Pdot, Qdot, Rdot";
+ }
+ if (SubSystems & ssVelocities) {
+ outstream << ", ";
+ outstream << "QBar, ";
+ outstream << "Vtotal, ";
+ outstream << "UBody, VBody, WBody, ";
+ outstream << "UAero, VAero, WAero, ";
+ outstream << "Vn, Ve, Vd";
+ }
+ if (SubSystems & ssForces) {
+ outstream << ", ";
+ outstream << "Drag, Side, Lift, ";
+ outstream << "L/D, ";
+ outstream << "Xforce, Yforce, Zforce";
+ }
+ if (SubSystems & ssMoments) {
+ outstream << ", ";
+ outstream << "L, M, N";
+ }
+ if (SubSystems & ssAtmosphere) {
+ outstream << ", ";
+ outstream << "Rho, ";
+ outstream << "NWind, EWind, DWind";
+ }
+ if (SubSystems & ssMassProps) {
+ outstream << ", ";
+ outstream << "Ixx, ";
+ outstream << "Iyy, ";
+ outstream << "Izz, ";
+ outstream << "Ixz, ";
+ outstream << "Mass, ";
+ outstream << "Xcg, Ycg, Zcg";
+ }
+ if (SubSystems & ssPosition) {
+ outstream << ", ";
+ outstream << "Altitude, ";
+ outstream << "Phi, Tht, Psi, ";
+ outstream << "Alpha, ";
+ outstream << "Beta, ";
+ outstream << "Latitude, ";
+ outstream << "Longitude, ";
+ outstream << "Distance AGL, ";
+ outstream << "Runway Radius";
+ }
+ if (SubSystems & ssCoefficients) {
+ outstream << ", ";
+ outstream << Aerodynamics->GetCoefficientStrings();
+ }
+ if (SubSystems & ssGroundReactions) {
+ outstream << ", ";
+ outstream << GroundReactions->GetGroundReactionStrings();
+ }
+ if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
+ outstream << ", ";
+ outstream << Propulsion->GetPropulsionStrings();
+ }
+
+ outstream << endl;
+ dFirstPass = false;
+ }
+
+ outstream << State->Getsim_time();
+ if (SubSystems & ssSimulation) {
+ }
+ if (SubSystems & ssAerosurfaces) {
+ outstream << ", ";
+ outstream << FCS->GetDaCmd() << ", ";
+ outstream << FCS->GetDeCmd() << ", ";
+ outstream << FCS->GetDrCmd() << ", ";
+ outstream << FCS->GetDaPos() << ", ";
+ outstream << FCS->GetDePos() << ", ";
+ outstream << FCS->GetDrPos();
+ }
+ if (SubSystems & ssRates) {
+ outstream << ", ";
+ outstream << Rotation->GetPQR() << ", ";
+ outstream << Rotation->GetPQRdot();
+ }
+ if (SubSystems & ssVelocities) {
+ outstream << ", ";
+ outstream << Translation->Getqbar() << ", ";
+ outstream << Translation->GetVt() << ", ";
+ outstream << Translation->GetUVW() << ", ";
+ outstream << Translation->GetvAeroUVW() << ", ";
+ outstream << Position->GetVel();
+ }
+ if (SubSystems & ssForces) {
+ outstream << ", ";
+ outstream << Aerodynamics->GetvFs() << ", ";
+ outstream << Aerodynamics->GetLoD() << ", ";
+ outstream << Aircraft->GetForces();
+ }
+ if (SubSystems & ssMoments) {
+ outstream << ", ";
+ outstream << Aircraft->GetMoments();
+ }
+ if (SubSystems & ssAtmosphere) {
+ outstream << ", ";
+ outstream << Atmosphere->GetDensity() << ", ";
+ outstream << Atmosphere->GetWindNED();
+ }
+ if (SubSystems & ssMassProps) {
+ outstream << ", ";
+ outstream << MassBalance->GetIxx() << ", ";
+ outstream << MassBalance->GetIyy() << ", ";
+ outstream << MassBalance->GetIzz() << ", ";
+ outstream << MassBalance->GetIxz() << ", ";
+ outstream << MassBalance->GetMass() << ", ";
+ 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 & ssCoefficients) {
+ outstream << ", ";
+ outstream << Aerodynamics->GetCoefficientValues();
+ }
+ if (SubSystems & ssGroundReactions) {
+ outstream << ", ";
+ outstream << GroundReactions->GetGroundReactionValues();
+ }
+ if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
+ outstream << ", ";
+ outstream << Propulsion->GetPropulsionValues();
}
- datafile << State->Getsim_time() << ",";
- datafile << Translation->Getqbar() << ",";
- datafile << Translation->GetVt() << ",";
- datafile << FCS->GetThrottlePos(0) << ",";
- datafile << FCS->GetDaPos() << ",";
- datafile << FCS->GetDePos() << ",";
- datafile << FCS->GetDrPos() << ",";
- datafile << Atmosphere->GetDensity() << ",";
- datafile << Aircraft->GetIxx() << ",";
- datafile << Aircraft->GetIyy() << ",";
- datafile << Aircraft->GetIzz() << ",";
- datafile << Aircraft->GetIxz() << ",";
- datafile << Aircraft->GetMass() << ",";
- datafile << Aircraft->GetXYZcg() << ",";
- datafile << Aircraft->GetForces() << ",";
- datafile << Aircraft->GetMoments() << ",";
- datafile << Position->Geth() << ",";
- datafile << Rotation->GetEuler() << ",";
- datafile << Rotation->GetPQR() << ",";
- datafile << Translation->GetUVW() << ",";
- datafile << Translation->Getalpha() << ",";
- datafile << Position->GetVel() << ",";
- datafile << Position->GetLatitude() << ",";
- datafile << Position->GetLongitude();
- datafile << endl;
- datafile.flush();
+ outstream << endl;
+ outstream.flush();
}
-/******************************************************************************/
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGOutput::SocketOutput(void)
{
string asciiData;
/*
- if (socket <= 0) return;
+ if (socket == NULL) return;
socket->Clear();
if (sFirstPass) {
socket->Append("Psi");
socket->Append("Rho");
socket->Append("Vtotal");
- socket->Append("U");
- socket->Append("V");
- socket->Append("W");
+ 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(Rotation->Getpsi());
socket->Append(Atmosphere->GetDensity());
socket->Append(Translation->GetVt());
- socket->Append(Translation->GetU());
- socket->Append(Translation->GetV());
- socket->Append(Translation->GetW());
+ socket->Append(Translation->GetUVW(eU));
+ socket->Append(Translation->GetUVW(eV));
+ socket->Append(Translation->GetUVW(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->Send(); */
}
-/******************************************************************************/
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGOutput::SocketStatusOutput(string out_str)
{
string asciiData;
- if (socket <= 0) return;
+ if (socket == NULL) return;
socket->Clear();
asciiData = string("<STATUS>") + out_str;
socket->Send();
}
-/******************************************************************************/
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+bool FGOutput::Load(FGConfigFile* AC_cfg)
+{
+ string token, parameter;
+ int OutRate = 0;
+
+ token = AC_cfg->GetValue("NAME");
+ Output->SetFilename(token);
+ token = AC_cfg->GetValue("TYPE");
+ Output->SetType(token);
+ 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