Journal of Control Science and Engineering / 2013 / Article / Tab 2

Research Article

Design of Attitude Control Systems for CubeSat-Class Nanosatellite

Table 2

Reaction wheel parameters.


Rotor mass0.214kg
Moment of inertia (axial)9.41 × 10−5Kg m2
Moment of inertia (transverse)5.02 × 10−5kg m2
Motor shaft Torque6.0 × 10−4N m
Maximum speed1539rad/s
Supply voltage3.7–4.2V

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