Coupling & Decoupling Control Study On Aircraft (Airbus A320)

The aim of this pro ect will be focused on creating two different types of flight controllers for the Airbus A320 using AT AB Simulink. The flight controller used for the aircraft has a decoupled flight controller and a coupled flight controller a decoupled flight controller means the longitudinal stability derivatives and lateral stability derivatives will have their own state-space dynamic model, but for the coupled flight controller the longitudinal stability derivatives and lateral stability derivatives will be combined together in order to create a new state-space dynamic model. In the last stages of this experiment, if both of the flight controllers are working perfectly and accurately, a user-friendly demo program manual will be produced for the potential user to compare the flight controller with other flight controllers or using this flight controller to control different types of aircraft. Therefore, an even better controller can be produced for the future potential user.