Research Article

Attitude Analysis of Small Satellites Using Model-Based Simulation

Table 2

Satellite description and simulation parameters.

3U CubeSat

Orbit406 km circular, 51.6° inclination
Mass
Inertia (, , )
4 kg
(0.0067, 0.0419, 0.0419) kg·m2
Permanent magnet dipole0.5 A·m2 along -axis
Angular rate dampingHysteresis: HyMu80 0.1 cm3 (0.05 cm3 along - and -axes)
Dimensions mm, no deployables
Simulation parameters0°/second initial rate
Simulation duration24 hours