Feedback Linearization of Quadrotor

Nowadays, unmanned aerial vehicles (UAVs) are growing exponentially in the sector of technology due to their flying ability. It helps in many sectors including military and civilian. Generally, MATLAB Simulink is used to analyze the system dynamically as it helps to analyze the system virtually. In this paper, first the mathematical model of quadrotor is derived, and then feedback linearization input-state technique is used on nonlinear rotational system to linearize the system and find new control inputs. Then, the system is simulated in MATLAB using the derived equations according to block diagram. To verify the result, plot function in MATLAB is used as it gives the graphical representation of the output.