Developement Of An Instrument Landing Simulation ... - Cal Poly

RThrust=RThrottle*Thrust;LThrust=LThrottle*Thrust;//printf("RThrust1-2: %i\n",RThrust);//printf("LThrust1-2: %i\n",LThrust);}}//Turboprop Engine: Engine Type = 2if (EngType == 2){Thrust=(Tsl*550)*(rho/rhosl)*(Np/(Vtrue*1.69)); //Tsl - eshpif (NumEng == 1){RThrust=0.5*RThrottle*Thrust;LThrust=0.5*RThrottle*Thrust;//printf("RThrust2-1: %i\n",RThrust);//printf("LThrust2-1: %i\n",LThrust);}else{RThrust=RThrottle*Thrust;LThrust=LThrottle*Thrust;//printf("RThrust2-2: %i\n",RThrust);//printf("LThrust2-2: %i\n",LThrust);}}69