DESIGN OF BACKSTEPPING SLIDING MODE CONTROLLER FOR QUADROTOR-TYPE UAV CONSIDERING MODEL UNCERTAINTY

Abstract

The paper presents the results of synthesizing the model of the Quadrotor
UAV, taking into account nonlinear constraints, model uncertainties and
aerodynamic disturbances. From there, an adaptive backstepping sliding
controller is used to ensure stability and sustainability. The results are
evaluated through simulation on Matlab-Simulink software, showing that the
controller has achieved the control quality requirements.