Application of guardian maps theory in flight control system design for aircraft model

With the development of the advanced technology, the flight control design faces more issues for meeting the complicated demands. The application of some stability theories in the flight control system is necessary to improve the generized peromances throughout the large flight envelop. This paper applies the guardian maps theory to the flight control law design by building the relations between the unknown parameters and the flight qualities. In the design process, for the fixed control structure, the control parameters can be adaptively obtained once the initial condition is determined. Finally, several illustrative examples are used in simulation to validate the feasibility of the proposed methods.