void IMS_PropulsionManager::SwitchThrusterMode(THRUSTER_HANDLE thruster, THRUSTERMODE *mode)
{
//calculate the flowrate so the injector can be updated accordingly, and remove the thruster from its injector
double maxmassflow = mode->Thrust / mode->Isp;
RemoveThruster(thruster, maxmassflow, false);
//get the propper injector for the new mode, or create it if necessary
vector<int> &thpropellants = mode->Propellants;
vector<float> &thratio = mode->Ratio;
double thefficiency = mode->Efficiency;
//set new properties for the thruster
vessel->SetThrusterIsp(thruster, mode->Isp);
vessel->SetThrusterMax0(thruster, mode->Thrust);
IMS_PropellantInjector *injector = getInjector(thpropellants, thratio, thefficiency);
injector->ConnectThruster(thruster, maxmassflow);
}
THRUSTER_HANDLE IMS_PropulsionManager::AddThruster(THRUSTERMODE *thrustermode, VECTOR3 &pos, VECTOR3 &dir)
{
vector<int> &thpropellants = thrustermode->Propellants;
vector<float> &thratio = thrustermode->Ratio;
double thefficiency = thrustermode->Efficiency;
//calculate position relative to CoG
VECTOR3 finalpos = pos + vessel->GetCoGmanager()->GetCoG();
THRUSTER_HANDLE newthruster = vessel->CreateThruster(pos, dir, thrustermode->Thrust, NULL, thrustermode->Isp);
double maxmassflow = thrustermode->Thrust / thrustermode->Isp;
//get a compatible injector, or create one if there isn't
IMS_PropellantInjector *injector = getInjector(thpropellants, thratio, thefficiency);
injector->ConnectThruster(newthruster, maxmassflow);
//add exhausts to the thruster
return newthruster;
}
int main(int argc, char *argv[]) {
return getInjector()->get<ShaderTool>()->startMainLoop(argc, argv);
}
int main(int argc, char *argv[]) {
getInjector()->get<Client>()->startMainLoop(argc, argv);
return EXIT_SUCCESS;
}
