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On-Orbit Center Of Mass Relocation System For A 3U Cubesat

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Figure

TABLE 1  UNITS FOR MAGENTIC PROPERTIES
Fig. 1. Coordinate systems for the CoM estimation: Orbital  Frame , with its origin in the CoM of the satellite,
TABLE 2 Parameters used onto simulink numerical simulations
Fig. 6. Satellite attitude with     [          ] cm. The simulation shows large oscillations in the attitude angles due to the disturbance torques, requiring that the attitude subsystem apply stabilization torques
+2

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