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

Table 3

Yaw angle controller performance indexes.

Items	SM	FSM without f and	FSM with f and
Reaction time (s)	0.201	0.214	0.215
Error (0.01 rad)	0.1	−0.07	0.37
Overshoot (0.01 rad)	0.12	0	0.4