Design of Attitude Control Systems for CubeSat-Class Nanosatellite

Table 2

Reaction wheel parameters.

Parameter	Value	Unit
Rotor mass	0.214	kg
Moment of inertia (axial)	9.41 × 10^−5	Kg m^2
Moment of inertia (transverse)	5.02 × 10^−5	kg m^2
Motor shaft Torque	6.0 × 10^−4	N m
Maximum speed	1539	rad/s
Supply voltage	3.7–4.2	V