Dynamic Modeling and Simple PID Control of Quadrotor UAV in Simulink

This project focuses on dynamic modeling and simple PID control implementation for quadrotor UAVs using Simulink. To achieve precise control and stable flight performance, we will develop a comprehensive dynamic model in Simulink that incorporates key physical parameters including mass properties, inertia matrix, and aerodynamic effects. The implementation will feature a multi-loop PID control structure addressing attitude stabilization (roll, pitch, yaw) and altitude control. Key Simulink blocks utilized will include transfer functions, state-space representations, and PID controller blocks with proper tuning parameters. The control algorithm will process sensor inputs through feedback loops to generate appropriate motor thrust commands. This approach enables thorough understanding of aircraft motion characteristics and facilitates accurate flight control. Through this project, we will establish fundamental skills in aircraft modeling and control system design using Simulink, providing a solid foundation for developing more advanced control algorithms and complex UAV designs in the future.