**5. Conclusions**

In this chapter, a fuzzy switching controller for the ADMIRE aircraft model has been developed and verification of the control scheme was conducted using MATLAB/Simulink. Here, a switching controller is designed for the stabilization of high-performance aircraft. To improve the switching controller performance, the fuzzy logic rule has been defined and used to obtain a robust stabilization control structure instead of a single conventional LQI and the switched LQI controller.

The proposed controller scheme was compared with the standard switched and the single conventional LQI controller for load-factor tracking and robust stability under the load-factor variations. The main conclusions of the simulation results are given as follows:

