Integrated Power and Attitude Control Design of Satellites Based on a Fuzzy Adaptive Disturbance Observer Using Variable-Speed Control Moment Gyros

Table 1

Nominal parameters and initial conditions of the simulation.

Symbol	Value	Unit
	4
	54.75	deg
		rad/s
		rad/s^2
		rad
		rad/s
		rad/s
		rad/s^2
		kg⋅m^2
		kg⋅m^2
,		kg⋅m^2
,		kg⋅m^2