RocketWorkbench/libsimulation/simulator/c++rocket.cc

#include <iostream>
#include <fstream.h>

#include "c++rocket.h"
#include "rocket.h"
#include "simulation.h"

//extern simulation *simptr;


int main(int argc, char *argv[]) {
 
  simulation muty(AERO_MODEL);
  
  simulation simple(SIMPLE_MODEL);
  
  //simptr = &muty;
  
  muty.set_propulseurs(1,"/home/antoine/debian/rocketsim-0.3/thrust/AEJ125.edx");
  muty.set_propulseurs(2,"/home/antoine/debian/rocketsim-0.3/thrust/AEJ180T.eng");
  //     muty.set_propulseurs(3,"/home/antoine/debian/rocketsim-0.3/thrust/AEK250W.eng");
  
  
  muty.set_prog(0,0,0);
  
  //cout << muty.tl[2] << endl;
  
  //simptr = &muty;
  
  double state[7] = {0, 0, 6370000, PI/3, PI/3, 100, 0};
  
  double state2[5] = {0, 0, 6370000, PI/3, 1000};
  //lsode ode;
  //int flag = ode.solve(state, 10, 0.1);
  
  
  
  muty.solve(state, 50, 0.01);
  
  simple.solve(state2, 1, 0.001);
  
  //     cout << simptr->prop[0].impulse() << endl;
  //     cout << simptr->prop[0].favg() << endl;
  //     cout << simptr->prop[0].vg() << endl;
  //     cout << simptr->prop[0].propellant_mass_fraction() << endl;
  //     cout << simptr->prop[0].impulse_to_weight() << endl;
  //     cout << simptr->prop[0].isp() << endl;
  
  

  //simptr->prop[0].plot_data();
  
  //for (int i = 0; i<MAXPROP; i++)
  //	  simptr->prop[i].print_data();
  

  //for (int i = 0; i < 40; i++)
  //	  cout << mass((double)i/2) << endl;
  
  
  //muty.print();
  //muty.export_octave("test");
  //simple.print();
  
  //ode.print();
  //simptr->print();
  
  
  //cout << flag << endl;
  

  return 0;
}