Improved Finite Control Set Optimal Control for PMSM in Rocket Launcher Servo System

Table 2

Step simulation data.

Control strategy	Adjustment time (s)	Maximum disturbance ()	Recovery time (s)	Steady-state error ()
IFCSOC	1.23	0.34	0.64	0.032
FCSOC	1.67	0.78	0.85	0.056