Modelling and PID Control System for Fixed-Wing Unmanned Aerial Vehicle
The paper focuses on the PID control techniques a for small UAV. In this research work, control derivatives were
implemented for analytical method for longitudinal dynamics of a small fixed wing UAV. The simulation results of
longitudinal stability derivatives have been proved for the UAV system with the help of MATLAB/SIMULINK model.
These methods can be used to convert the unstable conditions that cause by pole locations to stable conditions. And then the
PID controller can be used to adjust the desired set point for ARF 60 UAV.
Keywords – Modelling, Stability Analysis, Longitudinal Control, Fixed-wing UAV, MATLAB, SIMULINK model