Position Control of Quadcopter with First-Order Fast Nonsingular Terminal Sliding Mode Method

This paper discusses the position control and the design of the controller of unmanned aerial vehicles. We use the First-Order Fast Nonsingular Terminal Sliding Mode Control to design the dynamic function. Prove that the error of position and velocity can be convergence and don’t need to consider the Lyapunov function. We have made several simulations with the First-Order Fast Nonsingular Terminal Sliding Mode Control and prove that this design is feasible.