bool read_output_file(defaultEnsemble& ens, config& cfg){
if(cfg.valid("output") ) {
INFO_OUTPUT(1, "Loading from binary file " << cfg["output"]);
ens = swarm::snapshot::load(cfg["output"]);
INFO_OUTPUT(1,", time = " << ens.time_ranges() << endl);
return true;
}else if(cfg.valid("text_output")) {
INFO_OUTPUT(1, "Loading from text file " << cfg["text_output"]);
ens = swarm::snapshot::load_text(cfg["text_output"]);
INFO_OUTPUT(1,", time = " << ens.time_ranges() << endl);
return true;
}else
return false;
}
void prepare_integrator () {
// Initialize Integrator
DEBUG_OUTPUT(2, "Initializing integrator" );
double begin_time = initial_ens.time_ranges().average;
double destination_time = cfg.optional("destination_time", begin_time + 10 * M_PI );
integ = integrator::create(cfg);
integ->set_ensemble(current_ens);
integ->set_destination_time ( destination_time );
SYNC;
}
/**
* ***************TODO***********
*/
void replace_disabled_systems( defaultEnsemble& ens )
{
int nsys = ens.nsys();
// Replace the systems that have been disabled
for(int i = 0; i < nsys; i++)
{
if( ens[i].is_disabled() )
{
generate_initial_conditions_for_system(cfg,ens,i,maxsysid+1);
}
}
}
bool needs_shrinking( const defaultEnsemble& ens )
{
// This is the ratio we use when we are shrinking
// if the ratio of active ones to all is less
// than this number then we trim the fat
const double critical_ratio = 0.75;
int count_disabled = number_of_disabled_systems( ens ) ;
double ratio = double(count_disabled) / double( ens.nsys() );
return ratio > critical_ratio;
}
/**
* This is a very crucial part of the Monte Carlo simulation
* We remove the disabled ones and make a smaller ensemble.
* We don't really need to make another ensemble. But keeping
* the same ensemble is a lot of trouble.
*
*/
defaultEnsemble trim_disabled_systems( const defaultEnsemble& ens )
{
int nsys = ens.nsys();
int active_nsys = nsys - number_of_disabled_systems( ens ) ;
// WARNING: Needed to add this to prevent segfaults. TODO: Figure out why.
if(active_nsys==0) return ens;
int nbod = ens.nbod();
defaultEnsemble active_ens = defaultEnsemble::create( nbod, active_nsys );
// Copy the active ones to the new ensemble
for(int i = 0, j = 0; (i < nsys) && (j < active_nsys); i++)
{
if( !ens[i].is_disabled() )
{
ens[i].copyTo( active_ens[j] );
j++;
}
}
return active_ens;
}
void benchmark_item(const string& param, const string& value) {
//outputConfigSummary(std::cout,cfg);
if(!validate_configuration(cfg) ) ERROR( "Invalid configuration" );
if(param == "input" || param == "nsys" || param == "nbod" || cfg.count("reinitialize"))
load_generate_ensemble();
DEBUG_OUTPUT(2, "Make a copy of ensemble for energy conservation test" );
current_ens = initial_ens.clone();
double init_time = watch_time( prepare_integrator );
double integration_time = watch_time( generic_integrate );
double max_deltaE = find_max_energy_conservation_error(current_ens, initial_ens );
// Compare with reneference ensemble for integrator verification
double pos_diff = 0, vel_diff = 0, time_diff = 0;
bool comparison = compare_ensembles( current_ens, reference_ens , pos_diff, vel_diff, time_diff );
/// CSV output for use in spreadsheet software
std::cout << param << ", "
<< value << ", "
<< current_ens.time_ranges() << ", "
<< max_deltaE << ", "
<< pos_diff << ", "
<< vel_diff << ", "
<< time_diff << ", "
<< integration_time << ", "
<< init_time
<< std::endl;
if( !comparison || pos_diff > pos_threshold || vel_diff > vel_threshold || time_diff > time_threshold ){
fail_verify();
}
}
void run_integration(){
if(!validate_configuration(cfg) ) ERROR( "Invalid configuration" );
load_generate_ensemble();
DEBUG_OUTPUT(2, "Make a copy of ensemble for energy conservation test" );
current_ens = initial_ens.clone();
prepare_integrator();
double integration_time = watch_time ( cfg.valid("interval") ? stability_test : generic_integrate );
save_ensemble();
INFO_OUTPUT( 1, "Integration time: " << integration_time << " ms " << std::endl);
}
void write_stable_systems(defaultEnsemble &ens, defaultEnsemble &ens_init)
{
// find the stable ones and output the initial conditions for the stable
// ones in keplerian coordinates
// std::cerr << "# Finding stable system ids\n";
std::vector<unsigned int> stable_system_indices, unstable_system_indices;
for(int i = 0; i < ens.nsys() ; i++ )
{
if(ens[i].is_disabled())
unstable_system_indices.push_back(i);
else
stable_system_indices.push_back(i);
}
// std::cerr << "# Writing stable system ids\n";
if(cfg.count("stable_init_output"))
{
ofstream stable_init_output( cfg.optional("stable_init_output", string("stable_init_output.txt")).c_str() );
print_selected_systems(ens_init,stable_system_indices, stable_init_output);
}
if(cfg.count("stable_final_output"))
{
ofstream stable_final_output( cfg.optional("stable_final_output", string("stable_final_output.txt")).c_str() );
print_selected_systems(ens,stable_system_indices, stable_final_output);
}
if(cfg.count("unstable_init_output"))
{
ofstream unstable_init_output( cfg.optional("unstable_init_output", string("unstable_init_output.txt")).c_str() );
print_selected_systems(ens_init,unstable_system_indices, unstable_init_output);
}
if(cfg.count("unstable_final_output"))
{
ofstream unstable_final_output( cfg.optional("unstable_final_output", string("unstable_final_output.txt")).c_str() );
print_selected_systems(ens,unstable_system_indices, unstable_final_output);
}
}
void output_test() {
if(!validate_configuration(cfg) ) ERROR( "Invalid configuration" );
if(!read_input_file(initial_ens, cfg) ) {
ERROR("you should have a tested input file");
}
DEBUG_OUTPUT(2, "Make a copy of ensemble for energy conservation test" );
current_ens = initial_ens.clone();
prepare_integrator();
double integration_time = watch_time ( cfg.valid("interval") ? stability_test : generic_integrate );
if(read_output_file(reference_ens,cfg)){
// Compare with reneference ensemble for integrator verification
double pos_diff = 0, vel_diff = 0, time_diff = 0;
bool comparison = compare_ensembles( current_ens, reference_ens , pos_diff, vel_diff, time_diff );
INFO_OUTPUT(1,"\tPosition difference: " << pos_diff << endl
<< "\tVelocity difference: " << vel_diff << endl
<< "\tTime difference: " << time_diff << endl );
if( !comparison || pos_diff > pos_threshold || vel_diff > vel_threshold || time_diff > time_threshold ){
INFO_OUTPUT(0, "Test failed" << endl);
exit(1);
}else {
INFO_OUTPUT(0, "Test success" << endl);
}
}else{
ERROR("You should provide a test output file");
}
INFO_OUTPUT( 1, "Integration time: " << integration_time << " ms " << std::endl);
}
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
}
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();
}
}
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;
}
int number_of_disabled_systems(defaultEnsemble ens) {
int count_running = 0;
for(int i = 0; i < ens.nsys() ; i++)
if( ens[i].is_disabled() ) count_running++;
return count_running;
}
