Six-Degree-of-Freedom Uncontrolled Ballistic Missile Model

This MATLAB/Simulink implementation provides a six-degree-of-freedom uncontrolled ballistic missile model that simulates missile flight trajectories in the absence of control forces. The model employs fundamental flight dynamics equations including Newton-Euler equations for rigid body motion, aerodynamic coefficient calculations based on angle of attack and sideslip, and atmospheric density modeling. Through Simulink's RTW (Real-Time Workshop) capability, the model can be seamlessly converted to C/C++ code for real-time applications or embedded system deployment. This makes it particularly suitable for flight control students to learn trajectory simulation fundamentals, coordinate system transformations, and numerical integration methods. For extended learning, users can explore adding environmental factors like wind disturbances, varying atmospheric conditions, or implementing different flight modes to increase model complexity. Please feel free to post questions or suggestions. Happy learning