Design of a Fixed-Wing UAV Controller Combined Fuzzy Adaptive Method and Sliding Mode Control

Figure 6

Yaw angle-related signal comparison. (a) Yaw angle tracking comparison. (b) Yaw angle speed tracking comparison. (c) Yaw angle control input signal comparison. (d) Partial enlargement of Figure 6(a) at the first peak value.

(a)

(b)

(c)

(d)