Research Article
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 m2 | Moment of inertia (transverse) | 5.02 × 10−5 | kg m2 | Motor shaft Torque | 6.0 × 10−4 | N m | Maximum speed | 1539 | rad/s | Supply voltage | 3.7–4.2 | V |
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