This project is about implementing an LQG algorithm on a missile whose state model is partially unstable and implementing Guidance Navigation and Control logic to strike a missile on a given target coordinates. After making the required simulink model the mission is then implemented on FlightGear for visualization.
Youtube video - https://www.youtube.com/watch?v=0AJ6E48Aj9U&t=634s
Paper reference - https://www.researchgate.net/publication/303256153_Missile_Longitudinal_Autopilots_Connections_Between_Optimal_Control_and_Classical_Topologies