Backstepping Algorithm for Controlling of Quadrotor

In this paper, we consider the synthesis of a flight control system of an unmanned aerial vehicle like a quadrotor based on a backstepping procedure. The control object has a mathematical model in the form of the system of second-order differential equations, and it has essential nonlinear dynamics. The paper investigates a way of design the algorithm state feedback control based that stabilizing the final state. Some simulation results are presented, as well.