Research Article
Attitude Analysis of Small Satellites Using Model-Based Simulation
Table 2
Satellite description and simulation parameters.
| 3U CubeSat |
| Orbit | 406 km circular, 51.6° inclination | Mass Inertia (, , ) | 4 kg (0.0067, 0.0419, 0.0419) kg·m2 | Permanent magnet dipole | 0.5 A·m2 along -axis | Angular rate damping | Hysteresis: HyMu80 0.1 cm3 (0.05 cm3 along - and -axes) | Dimensions | mm, no deployables | Simulation parameters | 0°/second initial rate | Simulation duration | 24 hours |
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