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

LThrust=0.5*LThrottle*Thrust;//printf("RThrust4-1: %i\n",RThrust);//printf("LThrust4-1: %i\n",LThrust);}else{RThrust=RThrottle*Thrust;LThrust=LThrottle*Thrust;//printf("RThrust4-2: %i\n",RThrust);//printf("LThrust4-2: %i\n",LThrust);}}//Afterburning Jet Engine: Engine Type = 5if (EngType == 5){Thrust=Tsl*(rho/rhosl)*(1+0.7*(Vtrue*1.69/a)); //Tsl - lbsif (NumEng == 1){RThrust=0.5*RThrottle*Thrust;LThrust=0.5*LThrottle*Thrust;//printf("RThrust5-1: %i\n",RThrust);//printf("LThrust5-1: %i\n",LThrust);}else{RThrust=RThrottle*Thrust;71