Study of Quadcopter Movement Using CFD and PID with Numerical Methods

Quadcopters play a vital role in various industries due to their excellent maneuverability, enabling them to access hard-to-reach areas and perform tasks that traditional aircraft or vehicles cannot accomplish. The Quadcopter has 6-DoF movements that include both linear (x, y, z) and angular (roll, pitch, and yaw angles) motions. The study explores a new approach to study Quadcopter movement through the integration of Computational Fluid Dynamics, and proportional-integral-derivative with Numerical Methods. This work is useful to design a control system for the stability and maneuverability of quad-copter motion. In the present work, we developed mathematical models for quadcopter movement, simulated the models, and validated them using data from previous research. Our study is valuable for aviation system automation.