Research Article
Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications
Table 3
Results of PID controller based control actuation system.
| Parameters | Fuzzy PID | Conventional PID |
| Rise time— (ms) | 52.5 | 72.5 | Settling time— (ms) | 56.5 | 77.8 | Deceleration time— (ms) | 50.24 | 5.3 | Transient behavior | Smooth | Oscillatory | Peak overshoot | 2.7 | 13 | % error | 0.01 | 1.15 |
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