Attitude control of a quadcopter platform based on fractional control laws

الملخص EN

The purpose of this study, is to establish a comparison between two types of controllers, to be used to control the attitude of an unmanned aerial vehicle UAV, known as quadcopter platform.

The two types of controllers, assumed in this work, are: A classic Linear Quadratic Controller LQR, and Controller based on fractional control laws.

The proposed method shows its advantages in terms of time response and the settling down to the desired attitude, compared the LQR controller.