/******************************************************************************* 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 #include #include #ifdef HAVE_CURSES #include #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; } }