Application of Inverse Gauss Error Function to Attitude Control of Quadrotor

The attitude control problem and the controller design of quadrotor unmanned aerial vehicles (UAVs) based on SO(3) is discussed in this paper. We applied the special property of the inverse Gauss error function to the attitude error equation, and use the basic method that is the simplest way to converge, which the current attitude achieves the desired attitude. By numerical simulations, the controller based on SO(3) with inverse Gauss error function is exhibited and feasible.