A reaction wheel (110) detects an angular momentum. A satellite controller (120) selects a target thruster based on the detected angular momentum. A power supply apparatus (130) changes adjustment electric power for the target thruster. A flow rate adjustment apparatus (140) supplies a propellant to the target thruster at a flow rate corresponding to the adjustment electric power. This changes a thrust of the target thruster. When a discharge current of the target thruster does not become a target current, the power supply apparatus further changes the adjustment electric power for the target thruster.
ARTIFICIAL SATELLITE AND THRUST BALANCE ADJUSTMENT METHOD
KÜNSTLICHER SATELLIT UND VERFAHREN ZUM EINSTELLEN EINES SCHUBAUSGLEICHS
SATELLITE ARTIFICIEL ET PROCÉDÉ D'AJUSTEMENT DE BALANCE DE POUSSÉE
17.11.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Artificial satellite and thrust balance adjustment method
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