This project simulates the 3D attitude control of a quadcopter using PID controllers in MATLAB. The simulation numerically integrates the quadcopter’s nonlinear equations of motion using the ODE45 ...

Abstract: This paper presents practical results for PID tuning of a small-scale quadcopter through a series of flight experiments conducted on the roll, pitch, and yaw axes. Flight data were collected ...

Abstract: Quadcopter stability requires precise Proportional Integral Derivative (PID) tuning due to nonlinear flight dynamics. Traditional tuning methods struggle to balance stability, response speed ...