Determination of the speed parameter of flight control system by using adaptif network based fuzzy inference system

Flight control parameters have a very important task for a safe and quality flight of the air vehicles. In this study, ANFIS is used for determination of the flight parameters. The system modelled by ANFIS for Boeing B-737-300 type planes has four inputs (height, temperature in Fahrenheit, angle of flaps, weight) and one output (flying speed). The simulation results are comparatively presented for the real results.