Based on the original Rocket Workbench on SourceForge in CVS at:
https://sourceforge.net/projects/rocketworkbench
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78 lines
1.5 KiB
78 lines
1.5 KiB
#include <iostream>
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#include <fstream.h>
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#include "c++rocket.h"
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#include "rocket.h"
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#include "simulation.h"
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//extern simulation *simptr;
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int main(int argc, char *argv[]) {
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simulation muty(AERO_MODEL);
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simulation simple(SIMPLE_MODEL);
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//simptr = &muty;
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muty.set_propulseurs(1,"/home/antoine/debian/rocketsim-0.3/thrust/AEJ125.edx");
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muty.set_propulseurs(2,"/home/antoine/debian/rocketsim-0.3/thrust/AEJ180T.eng");
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// muty.set_propulseurs(3,"/home/antoine/debian/rocketsim-0.3/thrust/AEK250W.eng");
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muty.set_prog(0,0,0);
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//cout << muty.tl[2] << endl;
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//simptr = &muty;
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double state[7] = {0, 0, 6370000, PI/3, PI/3, 100, 0};
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double state2[5] = {0, 0, 6370000, PI/3, 1000};
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//lsode ode;
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//int flag = ode.solve(state, 10, 0.1);
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muty.solve(state, 50, 0.01);
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simple.solve(state2, 1, 0.001);
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// cout << simptr->prop[0].impulse() << endl;
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// cout << simptr->prop[0].favg() << endl;
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// cout << simptr->prop[0].vg() << endl;
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// cout << simptr->prop[0].propellant_mass_fraction() << endl;
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// cout << simptr->prop[0].impulse_to_weight() << endl;
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// cout << simptr->prop[0].isp() << endl;
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//simptr->prop[0].plot_data();
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//for (int i = 0; i<MAXPROP; i++)
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// simptr->prop[i].print_data();
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//for (int i = 0; i < 40; i++)
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// cout << mass((double)i/2) << endl;
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//muty.print();
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//muty.export_octave("test");
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//simple.print();
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//ode.print();
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//simptr->print();
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//cout << flag << endl;
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return 0;
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}
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