Research Article

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

Table 6

Airspeed controller performance indexes.

ItemsSMFSM without f and FSM with f and

Steady time (s)0.351.13.2
Steady error (m/s)āˆ’0.03āˆ’0.020.15
Overshoot (m/s)007.2