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

Table 4

Pitch angle controller performance indexes.

Items	SM	FSM without f and	FSM with f and
Reaction time (s)	0.211	0.232	0.234
Error (0.01 rad)	0.05	−0.12	0.41
Overshoot (0.01 rad)	0.09	0	0.43