Project 2: 6-DOF Dynamic Modeling & LQR Control System with HITL Validation

Project Goals: Build a complete 6-Degree-of-Freedom rigid-body flight dynamics model from first principles in MATLAB/Simulink, design state-space controllers (LQR with integral action and PID fallback), and validate control stability through Hardware-In-The-Loop (HITL) testing on a physical Pixhawk controller.