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