Control of the Lateral and Longitudinal Dynamics of UAV Quadcopter

Abstract

The research Unmanned Aerial Vehicles (UAV) has been considerably advanced. This work is interested principally in dynamic modeling of the four rotor mini aircraft named as a quadrotor. The dynamical model is obtained by Newton-Euler methodology. The robust controller is designed and simulated using a linear and nonlinear control techniques. Proportional Derivative Control and the Backstepping algorithm methods have been implemented in MATLAB/SIMULINK.