bool
ImR_Activator_i::still_running_i (const char *name, pid_t &pid)
{
bool is_running = this->running_server_list_.find (name) == 0;
if (is_running)
{
pid = ACE_INVALID_PID;
for (ProcessMap::ITERATOR iter = this->process_map_.begin ();
iter != process_map_.end ();
iter++)
{
if (ACE_OS::strcmp (name, iter->item ().c_str()) == 0)
{
pid = iter->key ();
break;
}
}
#if defined (ACE_WIN32)
if (pid != ACE_INVALID_PID)
{
Active_Pid_Setter aps(*this, pid);
pid_t waitp = this->process_mgr_.wait (pid, ACE_Time_Value::zero);
is_running = (waitp != pid);
}
#endif /* ACE_WIN32 */
}
return is_running;
}
int main() {
auto atmosphere = StE::Graphics::atmospherics_earth_properties({ 0,-6.371e+6,0 });
StE::Graphics::atmospherics_precompute_scattering aps(atmosphere);
// aps.load("atmospherics_scatter_lut.bin");
aps.build_optical_length_lut();
aps.build_scatter_lut(9);
aps.build_ambient_lut();
aps.write_out("atmospherics_scatter_lut.bin");
return 0;
}
/// Get the apriori solution, given the systems in the current epoch's data
Vector<double> getAprioriSolution(std::vector<SatID::SatelliteSystem> syss)
{
if(APSolution.size() == 3 + syss.size())
return APSolution;
// must cut down the vector
int j;
size_t i;
Vector<double> aps(3+syss.size(),0.0);
for(i=0; i<3; i++) aps[i] = APSolution[i];
for(j=3,i=0; i<APsysIDs.size(); i++) {
if(std::find(syss.begin(),syss.end(),APsysIDs[i]) != syss.end())
aps[j++] = APSolution[3+i];
}
return aps;
}
