Adaptive Robust Control and Active Vibration Suppression of Dumbbell-Shaped Spacecraft

Table 1

Parameters of dumbbell-shaped spacecraft.

Component	Items (unit)	Parameter
Main body	Mass (kg)	7000
	(m)
	Moment of inertia	Diag (6000,13000,13000)
Flexible beam	Mass (kg)	1600
	Moment of inertia	Diag (150,1.2e5,1.2e5)
	Nuclear reactor	Mass (kg)	3000
(m)
Moment of inertia		Diag (900,8000,8000)