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flightgear/JSBsim/FGOutput.cpp

214 lines
6.3 KiB
C++

/*******************************************************************************
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. 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.
HISTORY
--------------------------------------------------------------------------------
12/02/98 JSB Created
********************************************************************************
INCLUDES
*******************************************************************************/
#include <stdio.h>
#include <stdlib.h>
#include <iostream.h>
#ifdef HAVE_CURSES
#include <ncurses.h>
#endif
#include "FGOutput.h"
#include "FGState.h"
#include "FGFDMExec.h"
#include "FGAtmosphere.h"
#include "FGFCS.h"
#include "FGAircraft.h"
#include "FGTranslation.h"
#include "FGRotation.h"
#include "FGPosition.h"
#include "FGAuxiliary.h"
/*******************************************************************************
************************************ CODE **************************************
*******************************************************************************/
FGOutput::FGOutput(FGFDMExec* fdmex) : FGModel(fdmex)
{
strcpy(Name, "FGOutput");
FirstPass = true;
#ifdef HAVE_CURSES
initscr();
cbreak();
noecho();
#endif
}
FGOutput::~FGOutput(void)
{
}
bool FGOutput::Run(void)
{
if (!FGModel::Run()) {
DelimitedOutput();
// ConsoleOutput();
} else {
}
return false;
}
void FGOutput::ConsoleOutput(void)
{
#ifdef HAVE_CURSES
char buffer[20];
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");
move(3,1); sprintf(buffer,"%4.4f",Rotation->GetQ0()); insstr(buffer);
move(3,12); sprintf(buffer,"%4.4f",Rotation->GetQ1()); insstr(buffer);
move(3,23); sprintf(buffer,"%4.4f",Rotation->GetQ2()); insstr(buffer);
move(3,34); sprintf(buffer,"%4.4f",Rotation->GetQ3()); insstr(buffer);
move(0,0); insstr("Time: ");
move(0,6); insstr(gcvt(State->Getsim_time(),6,buffer));
move(2,46); insstr("Phi");
move(2,55); insstr("Tht");
move(2,64); insstr("Psi");
move(3,45); sprintf(buffer,"%3.3f",Rotation->Getphi()); insstr(buffer);
move(3,54); sprintf(buffer,"%3.3f",Rotation->Gettht()); insstr(buffer);
move(3,63); sprintf(buffer,"%3.3f",Rotation->Getpsi()); insstr(buffer);
move(5,47); insstr("U");
move(5,56); insstr("V");
move(5,65); insstr("W");
move(6,45); sprintf(buffer,"%5.2f",Translation->GetU()); insstr(buffer);
move(6,54); sprintf(buffer,"%5.2f",Translation->GetV()); insstr(buffer);
move(6,63); sprintf(buffer,"%5.2f",Translation->GetW()); insstr(buffer);
move(8,47); insstr("Fx");
move(8,56); insstr("Fy");
move(8,65); insstr("Fz");
move(9,45); sprintf(buffer,"%5.2f",Aircraft->GetFx()); insstr(buffer);
move(9,54); sprintf(buffer,"%5.2f",Aircraft->GetFy()); insstr(buffer);
move(9,63); sprintf(buffer,"%5.2f",Aircraft->GetFz()); insstr(buffer);
move(11,47); insstr("Fn");
move(11,56); insstr("Fe");
move(11,65); insstr("Fd");
move(12,45); sprintf(buffer,"%5.2f",Position->GetFn()); insstr(buffer);
move(12,54); sprintf(buffer,"%5.2f",Position->GetFe()); insstr(buffer);
move(12,63); sprintf(buffer,"%5.2f",Position->GetFd()); insstr(buffer);
move(14,47); insstr("Latitude");
move(14,57); insstr("Longitude");
move(14,67); insstr("Altitude");
move(15,47); sprintf(buffer,"%5.2f",State->Getlatitude()); insstr(buffer);
move(15,57); sprintf(buffer,"%5.2f",State->Getlongitude()); insstr(buffer);
move(15,67); sprintf(buffer,"%5.2f",State->Geth()); insstr(buffer);
refresh();
move(LINES-1,1);
refresh();
#endif
}
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 << 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 << endl;
}
}