Design of fuzzy inference system for estimating the flight control dynamics

This paper describes the design of Fuzzy Inference System to control the flight dynamic parameters of Unmanned Aerial Vehicle such as attitude [latitude, longitude and altitude], angles of rotation known as pitch and roll. A Soft Computing technique called Fuzzy Logic is used to design the Fuzzy Inference System. Visual simulation tool and Aerosim (Aeronautical Simulation Set) Flight gear interface are used for Simulation purpose.