R. J. Dev. Kwan eb05416991 Initial commit of "Rocket Workbench".
Taken from sources in CVS at:
    https://sourceforge.net/projects/rocketworkbench/

Sources extracted in two steps:
1. Pull entire project tree into a subdir "rwb" via "rsync":
    rsync -a a.cvs.sourceforge.net::cvsroot/rocketworkbench/ rwb/.
2. Export sources:
    export CVSROOT=$(pwd)/rwb
    SUBDIRS="analyser cpropep cpropep-web CVSROOT data libcompat libcpropep libnum libsimulation libthermo prop rocketworkbench rockflight"
    mkdir rwbx; cd rwbx
    cvs export -D now ${SUBDIRS}

After this (and some backups for safety), the directory content was
added to a Git repo:
    git init .
    git add *
2021-01-20 15:50:36 -08:00

79 lines
1.5 KiB
C++

#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;
}