“…Usually, the linearization method used to get a set of equivalent linear models based on the state points in entire envelope, then, we could design the controllers on linear system theory according to the flight criterion of different aircraft [12]. Obviously, its disadvantage is evident that every controller must ensure the system stable on each flight state point and also around its little region, and must be smoothly switched the controller to another flight state point, this is not easy in LFE, So, kinds of control methods, such as fuzzy logic, adaptive control, neural network, H ∞ control so on, proposed to solve this problems [13][14][15][16][17][18], and many of them took on a effective result. This paper try to apply H∞ mixed fuzzy output feedback control, and by means of the different stability condition in [19] to introduce a variable and design a different controller from [6,11] in flight control law.…”