Research Article
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 |
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