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

Table 5

Roll angle controller performance indexes.

Items	SM	FSM without f and	FSM with f and
Reaction time (s)	0.198	0.219	0.221
Error (0.01 rad)	−0.03	−0.32	0.19
Overshoot (0.01 rad)	0.01	0.35	0.39