The job is as the title. I have a basic system that has an airfoil with a flap and need to achieve a set height based on the flap angle. I need a Simulink transfer function that takes the output vertical force, converts it too a vertical displacement and then controls the angle the flap.
I have 3dof systems (2 forces, 1 moment) that needs to be presented in state space form. This is aerodynamic type system