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
--------------------------------------------------------------------------------
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 "FGPosition.h"
#include "FGAuxiliary.h"
+static const char *IdSrc = "$Header$";
+static const char *IdHdr = ID_OUTPUT;
+
/*******************************************************************************
************************************ CODE **************************************
*******************************************************************************/
FGOutput::FGOutput(FGFDMExec* fdmex) : FGModel(fdmex)
{
Name = "FGOutput";
- FirstPass = true;
-#ifdef HAVE_CURSES
- initscr();
- cbreak();
- noecho();
+ 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
}
+/******************************************************************************/
FGOutput::~FGOutput(void)
{
+ if (socket) delete socket;
}
+/******************************************************************************/
bool FGOutput::Run(void)
{
- if (!FGModel::Run()) {
- DelimitedOutput();
-// ConsoleOutput();
- } else {
+ if (enabled) {
+ if (!FGModel::Run()) {
+
+ if (Type == otSocket) {
+ SocketOutput();
+ } else if (Type == otCSV) {
+ if (Filename != "COUT" && Filename != "cout" && Filename.size() > 0) {
+ DelimitedOutput(Filename);
+ } else {
+ DelimitedOutput();
+ }
+ } 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::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;
+ } else if (type == "TABULAR") {
+ Type = otTab;
+ } else if (type == "SOCKET") {
+ Type = otSocket;
+ } else if (type == "TERMINAL") {
+ Type = otTerminal;
+ } else if (type != "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(void)
+{
+ if (dFirstPass) {
+ cout << "Time";
+ if (SubSystems & FGAircraft::ssSimulation) {
+ // Nothing here, yet
+ }
+ if (SubSystems & FGAircraft::ssAerosurfaces) {
+ cout << ", ";
+ cout << "Throttle, ";
+ cout << "Aileron Cmd, ";
+ cout << "Elevator Cmd, ";
+ cout << "Rudder Cmd, ";
+ cout << "Aileron Pos, ";
+ cout << "Elevator Pos, ";
+ cout << "Rudder Pos";
+ }
+ if (SubSystems & FGAircraft::ssRates) {
+ cout << ", ";
+ cout << "P, Q, R";
+ }
+ if (SubSystems & FGAircraft::ssVelocities) {
+ cout << ", ";
+ cout << "QBar, ";
+ cout << "Vtotal, ";
+ cout << "U, V, W, ";
+ cout << "Vn, Ve, Vd";
+ }
+ if (SubSystems & FGAircraft::ssForces) {
+ cout << ", ";
+ cout << "XsForce, YsForce, ZsForce, ";
+ cout << "Xforce, Yforce, Zforce";
+ }
+ if (SubSystems & FGAircraft::ssMoments) {
+ cout << ", ";
+ cout << "L, M, N";
+ }
+ if (SubSystems & FGAircraft::ssAtmosphere) {
+ cout << ", ";
+ cout << "Rho";
+ }
+ if (SubSystems & FGAircraft::ssMassProps) {
+ cout << ", ";
+ cout << "Ixx, ";
+ cout << "Iyy, ";
+ cout << "Izz, ";
+ cout << "Ixz, ";
+ cout << "Mass, ";
+ cout << "Xcg, Ycg, Zcg";
+ }
+ if (SubSystems & FGAircraft::ssPosition) {
+ cout << ", ";
+ cout << "Altitude, ";
+ cout << "Phi, Tht, Psi, ";
+ cout << "Alpha, ";
+ cout << "Latitude, ";
+ cout << "Longitude, ";
+ cout << "Distance AGL, ";
+ cout << "Runway Radius";
+ }
+ if (SubSystems & FGAircraft::ssCoefficients) {
+ cout << ", ";
+ cout << Aircraft->GetCoefficientStrings();
+ }
+ if (SubSystems & FGAircraft::ssGroundReactions) {
+ cout << ", ";
+ cout << Aircraft->GetGroundReactionStrings();
+ }
- move(2,46); insstr("Phi");
- move(2,55); insstr("Tht");
- move(2,64); insstr("Psi");
+ cout << endl;
+ dFirstPass = false;
+ }
- 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());
+ cout << State->Getsim_time();
+ if (SubSystems & FGAircraft::ssSimulation) {
+ }
+ if (SubSystems & FGAircraft::ssAerosurfaces) {
+ cout << ", ";
+ cout << FCS->GetThrottlePos(0) << ", ";
+ cout << FCS->GetDaCmd() << ", ";
+ cout << FCS->GetDeCmd() << ", ";
+ cout << FCS->GetDrCmd() << ", ";
+ cout << FCS->GetDaPos() << ", ";
+ cout << FCS->GetDePos() << ", ";
+ cout << FCS->GetDrPos();
+ }
+ if (SubSystems & FGAircraft::ssRates) {
+ cout << ", ";
+ cout << Rotation->GetPQR();
+ }
+ if (SubSystems & FGAircraft::ssVelocities) {
+ cout << ", ";
+ cout << Translation->Getqbar() << ", ";
+ cout << Translation->GetVt() << ", ";
+ cout << Translation->GetUVW() << ", ";
+ cout << Position->GetVel();
+ }
+ if (SubSystems & FGAircraft::ssForces) {
+ cout << ", ";
+ cout << Aircraft->GetvFs() << ", ";
+ cout << Aircraft->GetForces();
+ }
+ if (SubSystems & FGAircraft::ssMoments) {
+ cout << ", ";
+ cout << Aircraft->GetMoments();
+ }
+ if (SubSystems & FGAircraft::ssAtmosphere) {
+ cout << ", ";
+ cout << Atmosphere->GetDensity();
+ }
+ if (SubSystems & FGAircraft::ssMassProps) {
+ cout << ", ";
+ cout << Aircraft->GetIxx() << ", ";
+ cout << Aircraft->GetIyy() << ", ";
+ cout << Aircraft->GetIzz() << ", ";
+ cout << Aircraft->GetIxz() << ", ";
+ cout << Aircraft->GetMass() << ", ";
+ cout << Aircraft->GetXYZcg();
+ }
+ if (SubSystems & FGAircraft::ssPosition) {
+ cout << ", ";
+ cout << Position->Geth() << ", ";
+ cout << Rotation->GetEuler() << ", ";
+ cout << Translation->Getalpha() << ", ";
+ cout << Position->GetLatitude() << ", ";
+ cout << Position->GetLongitude() << ", ";
+ cout << Position->GetDistanceAGL() << ", ";
+ cout << Position->GetRunwayRadius();
+ }
+ if (SubSystems & FGAircraft::ssCoefficients) {
+ cout << ", ";
+ cout << Aircraft->GetCoefficientValues();
+ }
+ if (SubSystems & FGAircraft::ssGroundReactions) {
+ cout << ", ";
+ cout << Aircraft->GetGroundReactionValues();
+ }
+ cout << endl;
+}
- move(5,47); insstr("U");
- move(5,56); insstr("V");
- move(5,65); insstr("W");
+/******************************************************************************/
- 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());
+void FGOutput::DelimitedOutput(string fname)
+{
+ if (sFirstPass) {
+ datafile.open(fname.c_str());
+ datafile << "Time";
+ if (SubSystems & FGAircraft::ssSimulation) {
+ // Nothing here, yet
+ }
+ if (SubSystems & FGAircraft::ssAerosurfaces) {
+ datafile << ", ";
+ datafile << "Throttle, ";
+ datafile << "Aileron Cmd, ";
+ datafile << "Elevator Cmd, ";
+ datafile << "Rudder Cmd, ";
+ datafile << "Aileron Pos, ";
+ datafile << "Elevator Pos, ";
+ datafile << "Rudder Pos";
+ }
+ if (SubSystems & FGAircraft::ssRates) {
+ datafile << ", ";
+ datafile << "P, Q, R";
+ }
+ if (SubSystems & FGAircraft::ssVelocities) {
+ datafile << ", ";
+ datafile << "QBar, ";
+ datafile << "Vtotal, ";
+ datafile << "U, V, W, ";
+ datafile << "Vn, Ve, Vd";
+ }
+ if (SubSystems & FGAircraft::ssForces) {
+ datafile << ", ";
+ datafile << "XsForce, YsForce, ZsForce, ";
+ datafile << "Xforce, Yforce, Zforce";
+ }
+ if (SubSystems & FGAircraft::ssMoments) {
+ datafile << ", ";
+ datafile << "L, M, N";
+ }
+ if (SubSystems & FGAircraft::ssAtmosphere) {
+ datafile << ", ";
+ datafile << "Rho";
+ }
+ if (SubSystems & FGAircraft::ssMassProps) {
+ datafile << ", ";
+ datafile << "Ixx, ";
+ datafile << "Iyy, ";
+ datafile << "Izz, ";
+ datafile << "Ixz, ";
+ datafile << "Mass, ";
+ datafile << "Xcg, Ycg, Zcg";
+ }
+ if (SubSystems & FGAircraft::ssPosition) {
+ datafile << ", ";
+ datafile << "Altitude, ";
+ datafile << "Phi, Tht, Psi, ";
+ datafile << "Alpha, ";
+ datafile << "Latitude, ";
+ datafile << "Longitude, ";
+ datafile << "Distance AGL, ";
+ datafile << "Runway Radius";
+ }
+ if (SubSystems & FGAircraft::ssCoefficients) {
+ datafile << ", ";
+ datafile << Aircraft->GetCoefficientStrings();
+ }
+ if (SubSystems & FGAircraft::ssGroundReactions) {
+ datafile << ", ";
+ datafile << Aircraft->GetGroundReactionStrings();
+ }
+ datafile << endl;
+ sFirstPass = false;
+ }
- move(8,47); insstr("Fx");
- move(8,56); insstr("Fy");
- move(8,65); insstr("Fz");
+ datafile << State->Getsim_time();
+ if (SubSystems & FGAircraft::ssSimulation) {
+ }
+ if (SubSystems & FGAircraft::ssAerosurfaces) {
+ datafile << ", ";
+ datafile << FCS->GetThrottlePos(0) << ", ";
+ datafile << FCS->GetDaCmd() << ", ";
+ datafile << FCS->GetDeCmd() << ", ";
+ datafile << FCS->GetDrCmd() << ", ";
+ datafile << FCS->GetDaPos() << ", ";
+ datafile << FCS->GetDePos() << ", ";
+ datafile << FCS->GetDrPos();
+ }
+ if (SubSystems & FGAircraft::ssRates) {
+ datafile << ", ";
+ datafile << Rotation->GetPQR();
+ }
+ if (SubSystems & FGAircraft::ssVelocities) {
+ datafile << ", ";
+ datafile << Translation->Getqbar() << ", ";
+ datafile << Translation->GetVt() << ", ";
+ datafile << Translation->GetUVW() << ", ";
+ datafile << Position->GetVel();
+ }
+ if (SubSystems & FGAircraft::ssForces) {
+ datafile << ", ";
+ datafile << Aircraft->GetvFs() << ", ";
+ datafile << Aircraft->GetForces();
+ }
+ if (SubSystems & FGAircraft::ssMoments) {
+ datafile << ", ";
+ datafile << Aircraft->GetMoments();
+ }
+ if (SubSystems & FGAircraft::ssAtmosphere) {
+ datafile << ", ";
+ datafile << Atmosphere->GetDensity();
+ }
+ if (SubSystems & FGAircraft::ssMassProps) {
+ datafile << ", ";
+ datafile << Aircraft->GetIxx() << ", ";
+ datafile << Aircraft->GetIyy() << ", ";
+ datafile << Aircraft->GetIzz() << ", ";
+ datafile << Aircraft->GetIxz() << ", ";
+ datafile << Aircraft->GetMass() << ", ";
+ datafile << Aircraft->GetXYZcg();
+ }
+ if (SubSystems & FGAircraft::ssPosition) {
+ datafile << ", ";
+ datafile << Position->Geth() << ", ";
+ datafile << Rotation->GetEuler() << ", ";
+ datafile << Translation->Getalpha() << ", ";
+ datafile << Position->GetLatitude() << ", ";
+ datafile << Position->GetLongitude() << ", ";
+ datafile << Position->GetDistanceAGL() << ", ";
+ datafile << Position->GetRunwayRadius();
+ }
+ if (SubSystems & FGAircraft::ssCoefficients) {
+ datafile << ", ";
+ datafile << Aircraft->GetCoefficientValues();
+ }
+ if (SubSystems & FGAircraft::ssGroundReactions) {
+ datafile << ", ";
+ datafile << Aircraft->GetGroundReactionValues();
+ }
+ datafile << endl;
+ datafile.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;
+
+ 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("U");
+ socket->Append("V");
+ socket->Append("W");
+ 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");
+ socket->Append("Longitude");
+ socket->Append("QBar");
+ socket->Append("Alpha");
+ socket->Append("L");
+ socket->Append("M");
+ socket->Append("N");
+ socket->Append("Throttle");
+ socket->Append("Aileron");
+ socket->Append("Elevator");
+ socket->Append("Rudder");
+ 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(Position->Geth());
+ socket->Append(Rotation->Getphi());
+ socket->Append(Rotation->Gettht());
+ 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(Position->GetVn());
+ socket->Append(Position->GetVe());
+ socket->Append(Position->GetVd());
+ socket->Append(Translation->GetUdot());
+ socket->Append(Translation->GetVdot());
+ socket->Append(Translation->GetWdot());
+ socket->Append(Rotation->GetP());
+ socket->Append(Rotation->GetQ());
+ socket->Append(Rotation->GetR());
+ socket->Append(Rotation->GetPdot());
+ socket->Append(Rotation->GetQdot());
+ socket->Append(Rotation->GetRdot());
+ socket->Append(Aircraft->GetFx());
+ socket->Append(Aircraft->GetFy());
+ socket->Append(Aircraft->GetFz());
+ socket->Append(Position->GetLatitude());
+ socket->Append(Position->GetLongitude());
+ socket->Append(Translation->Getqbar());
+ socket->Append(Translation->Getalpha());
+ socket->Append(Aircraft->GetL());
+ socket->Append(Aircraft->GetM());
+ socket->Append(Aircraft->GetN());
+ socket->Append(FCS->GetThrottle(0));
+ socket->Append(FCS->GetDa());
+ socket->Append(FCS->GetDe());
+ socket->Append(FCS->GetDr());
+ socket->Send(); */
+}
- 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)
-{
- 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;
- } 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;
- }
-}
projects / flightgear.git / blobdiff