DESIGN OF SLIDING MODE CONTROLLER FOR UAV STYLE QUADROTOR

Abstract

The article presents the results of synthesizing the model of the Quadrotor,
taking into account geometric nonlinear constraints, as well as physical
phenomena affecting the kinematics of the flying device. From there, use the
sliding mode controller to ensure stability and sustainability against noise. The
results of the article are evaluated through simulation on Matlab-Simulink
software, showing that the controller has achieved flight quality requirements.