Adaptive Fuzzy Control for Attitude Stabilization of Spacecraft with Deployable Composite Laminated Solar Array

Table 2

Parameters of the PD controller in the simulation cases.

Group list	Case list	KP	KD
Group 1	Case 1	6.5	12.5
	Case 2	12.0	12.5
	Case 3	17.0	12.5
Group 2	Case 1	17.0	5.5
	Case 2	17.0	12.5
	Case 3	17.0	25.6