std::vector<std::vector<double> > calc_semimajor_axes(defaultEnsemble& ens)
{
std::vector<std::vector<double> > semimajor_axes(ens.nsys(),std::vector<double>(ens.nbod(),0.));
for(int sys_idx = 0; sys_idx < ens.nsys() ; sys_idx++)
{
int sys_id = ens[sys_idx].id();
assert(sys_id>=0);
assert(sys_id<ens.nsys());
double star_mass = ens.mass(sys_idx,0);
double mass_effective = star_mass;
double bx, by, bz, bvx, bvy, bvz;
ens.get_barycenter(sys_idx,bx,by,bz,bvx,bvy,bvz,0);
for(unsigned int bod=1;bod<ens.nbod();++bod) // Skip star since calculating orbits
{
double mass = ens.mass(sys_idx,bod);
mass_effective += mass;
ens.get_barycenter(sys_idx,bx,by,bz,bvx,bvy,bvz,bod-1);
double x = ens.x(sys_idx,bod)-bx;
double y = ens.y(sys_idx,bod)-by;
double z = ens.z(sys_idx,bod)-bz;
double vx = ens.vx(sys_idx,bod)-bvx;
double vy = ens.vy(sys_idx,bod)-bvy;
double vz = ens.vz(sys_idx,bod)-bvz;
double a, e, i, O, w, M;
calc_keplerian_for_cartesian(a,e,i,O,w,M, x,y,z,vx,vy,vz, mass_effective);
semimajor_axes[sys_id][bod-1] = a;
}
}
return semimajor_axes;
}
void disable_unstable_systems(defaultEnsemble& ens, const std::vector<std::vector<double> >& semimajor_axes_init, const double deltaa_threshold )
{
for(int sys_idx = 0; sys_idx < ens.nsys() ; sys_idx++)
{
if(ens[sys_idx].is_disabled() ) continue;
bool disable = false;
int sys_id = ens[sys_idx].id();
double star_mass = ens.mass(sys_idx,0);
double mass_effective = star_mass;
double bx, by, bz, bvx, bvy, bvz;
ens.get_barycenter(sys_idx,bx,by,bz,bvx,bvy,bvz,0);
for(unsigned int bod=1;bod<ens.nbod();++bod) // Skip star since calculating orbits
{
// std::cout << "body= " << bod << ": ";
// std::cout << "pos= (" << ens.x(sys_idx, bod) << ", " << ens.y(sys_idx, bod) << ", " << ens.z(sys_idx, bod) << ") vel= (" << ens.vx(sys_idx, bod) << ", " << ens.vy(sys_idx, bod) << ", " << ens.vz(sys_idx, bod) << ").\n";
double mass = ens.mass(sys_idx,bod);
mass_effective += mass;
ens.get_barycenter(sys_idx,bx,by,bz,bvx,bvy,bvz,bod-1);
double x = ens.x(sys_idx,bod)-bx;
double y = ens.y(sys_idx,bod)-by;
double z = ens.z(sys_idx,bod)-bz;
double vx = ens.vx(sys_idx,bod)-bvx;
double vy = ens.vy(sys_idx,bod)-bvy;
double vz = ens.vz(sys_idx,bod)-bvz;
double a, e, i, O, w, M;
calc_keplerian_for_cartesian(a,e,i,O,w,M, x,y,z,vx,vy,vz, mass_effective);
i *= 180/M_PI;
O *= 180/M_PI;
w *= 180/M_PI;
M *= 180/M_PI;
if(!((e>=0.)&&(e<1.0))) { disable = true; }
if(!((a>0.)&&(a<10.0))) { disable = true; }
assert(sys_id>=0);
assert(sys_id<semimajor_axes_init.size());
assert(bod-1>=0);
assert(bod-1<semimajor_axes_init[sys_id].size());
double da = a - semimajor_axes_init[sys_id][bod-1];
if(fabs(da) >= deltaa_threshold * semimajor_axes_init[sys_id][bod-1])
{ disable = true; }
if(disable)
{
if(cfg.count("verbose"))
std::cout << "# Disabling idx=" << sys_idx << " id=" << sys_id << " b=" << bod << " a= " << a << " e= " << e << " i= " << i << " Omega= " << O << " omega= " << w << " M= " << M << "\n";
break;
}
}
if(disable) ens[sys_idx].set_disabled();
}
}
void generate_initial_conditions_for_system(const config& cfg, defaultEnsemble &ens, const int sysidx, const int sysid)
{
double time_init = cfg.optional("time_init", 0.0);
const bool use_jacobi = cfg.optional("use_jacobi", 0);
bool keplerian_ephemeris = cfg.optional("use_keplerian", 1);
bool transit_ephemeris = cfg.optional("use_transit", 0);
if(transit_ephemeris) keplerian_ephemeris = 0;
assert(!(keplerian_ephemeris && transit_ephemeris)); // find a better way
ens[sysidx].id() = sysid;
ens[sysidx].time() = time_init;
ens[sysidx].set_active();
if(sysid>maxsysid) maxsysid = sysid;
// set sun to unit mass and at origin
double mass_star = draw_value_from_config(cfg,"mass_star",0.00003,100.);
double x=0, y=0, z=0, vx=0, vy=0, vz=0;
ens.set_body(sysidx, 0, mass_star, x, y, z, vx, vy, vz);
// If omitted or value of zero, then default to cycling through body id to make eccentric
int ecc_body = cfg.optional("ecc_body", 0);
if(ecc_body==0)
{ ecc_body = 1+(sysid*(ens.nbod()-1))/ens.nsys(); }
double mass_enclosed = mass_star;
for(unsigned int bod=1;bod<ens.nbod();++bod)
{
double mass_planet = draw_value_from_config(cfg,"mass",bod,0.,mass_star);
mass_enclosed += mass_planet;
double a, e, i, O, w, M;
if(transit_ephemeris)
{
double period = draw_value_from_config(cfg,"period",bod,0.2,365250.);
double epoch = draw_value_from_config(cfg,"epoch",bod,0.2,365250.);
a = pow((period/365.25)*(period/365.25)*mass_enclosed,1.0/3.0);
if(bod==ecc_body)
e = draw_value_from_config(cfg,"ecc",bod,0.,1.);
else
e = 0.;
i = draw_value_from_config(cfg,"inc",bod,-180.,180.);
O = draw_value_from_config(cfg,"node",bod,-720.,720.);
w = draw_value_from_config(cfg,"omega",bod,-720.,720.);
i *= M_PI/180.;
O *= M_PI/180.;
w *= M_PI/180.;
double T = (0.5*M_PI-w)+2.0*M_PI*((epoch/period)-floor(epoch/period));
double E = atan2(sqrt(1.-e)*(1.+e)*sin(T),e+cos(T));
M = E-e*sin(E);
}
else if (keplerian_ephemeris)
{
a = draw_value_from_config(cfg,"a",bod,0.001,10000.);
if(bod==ecc_body)
e = draw_value_from_config(cfg,"ecc",bod,0.,1.);
else
e = 0.;
i = draw_value_from_config(cfg,"inc",bod,-180.,180.);
O = draw_value_from_config(cfg,"node",bod,-720.,720.);
w = draw_value_from_config(cfg,"omega",bod,-720.,720.);
M = draw_value_from_config(cfg,"meananom",bod,-720.,720.);
i *= M_PI/180.;
O *= M_PI/180.;
w *= M_PI/180.;
M *= M_PI/180.;
}
double mass = use_jacobi ? mass_enclosed : mass_star+mass_planet;
if(cfg.count("verbose")&&(sysid<10))
std::cout << "# Drawing sysid= " << sysid << " bod= " << bod << ' ' << mass_planet << " " << a << ' ' << e << ' ' << i*180./M_PI << ' ' << O*180./M_PI << ' ' << w*180./M_PI << ' ' << M*180./M_PI << '\n';
calc_cartesian_for_ellipse(x,y,z,vx,vy,vz, a, e, i, O, w, M, mass);
// printf("%d %d: %lg (%lg %lg %lg) (%lg %lg %lg) \n", sysidx, bod, mass_planet, x,y,z,vx,vy,vz);
if(use_jacobi)
{
double bx, by, bz, bvx, bvy, bvz;
ens.get_barycenter(sysidx,bx,by,bz,bvx,bvy,bvz,bod-1);
x += bx; y += by; z += bz;
vx += bvx; vy += bvy; vz += bvz;
}
// assign body a mass, position and velocity
ens.set_body(sysidx, bod, mass_planet, x, y, z, vx, vy, vz);
if(cfg.count("verbose")&&(sysid<10))
{
double x_t = ens.x(sysidx,bod);
double y_t = ens.y(sysidx,bod);
double z_t = ens.z(sysidx,bod);
double vx_t = ens.vx(sysidx,bod);
double vy_t = ens.vy(sysidx,bod);
double vz_t = ens.vz(sysidx,bod);
std::cout << " x= " << x << "=" << x_t << " ";
std::cout << " y= " << y << "=" << y_t << " ";
std::cout << " z= " << z << "=" << z_t << " ";
std::cout << "vx= " << vx << "=" << vx_t << " ";
std::cout << "vy= " << vy << "=" << vy_t << " ";
std::cout << "vz= " << vz << "=" << vz_t << "\n";
}
} // end loop over bodies
// Shift into barycentric frame
ens.get_barycenter(sysidx,x,y,z,vx,vy,vz);
for(unsigned int bod=0;bod<ens.nbod();++bod)
{
ens.set_body(sysidx, bod, ens.mass(sysidx,bod),
ens.x(sysidx,bod)-x, ens.y(sysidx,bod)-y, ens.z(sysidx,bod)-z,
ens.vx(sysidx,bod)-vx, ens.vy(sysidx,bod)-vy, ens.vz(sysidx,bod)-vz);
} // end loop over bodies
}
