Generic Model of a Satellite Attitude Control System

Table 1

Satellite mass properties.

Description	Value	Unit
Mass	6.2	[kg]
Moments of inertia: , ,	0.0756, 0.0763, 0.0209	[kg·m^2]
Products of inertia: , ,	-0.0002, 0.0020, -0.0019	[kg·m^2]
Location of center of mass relative to geometrical center (, , )	0.0034, -0.0036, -0.0007	[m]
Dimensions		[m]