Embedded Super Twisting Control for the Attitude of a Quadrotor

This paper focuses on the embedded super twisting control for the orientation dynamics of a quadrotor. The Newton-Euler approach is applied to obtain the dynamic model of the quadrotor and a functional description of the experimental platform is described. In order to implement the control algorithm and perform real-time flights, a commercial flight computer is used. Experimental results are obtained in real-time during the autonomous flight.