DESIGN OF A QUADROTOR POSITION CONTROLLER USING FEEDBACK LINEARIZED METHOD

Abstract

This article presents a method for designing a nonlinear quadrotor
Unmanned Aerial Vehicle (UAV) controller, based on dividing the quadrotor's
dynamic model into structurally dependent subsystems and using routes.
feedback calculation. Based on the synthesized controllers, simulate the
quadrotor position control system using Matlab-Simulink. The simulation
results demonstrate the correctness of the algorithm and approach when
synthesizing the complex controller of the quadrotor.