Design of Fuzzy controller for tracking of desired trajectory of 2-DOF Aero System

This paper presents a unique design of fuzzy controller, used for attitude control of a two Degrees of freedom Aero flight control simulator. The proposed controller utilizes a parallel structure of Mamdani fuzzy system to track the attitude and overcome parametric uncertainties due to coupled dynamics of the system. To validate the proposed design, numerical simulations are carried out and been compared with existing methods. The tracking responses of yaw and pitch point out fast convergence of error with minimum overshoot in the presence of unmatched uncertainties.