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Published in 2019 at "IEEE Access"
DOI: 10.1109/access.2019.2922705
Abstract: A control moment gyro (CMG) is the main source of vibration disturbance in the spacecraft. This paper presents a vibration mathematical model with 18 degrees of freedom by Lagrange energy method, for solving the problem…
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Keywords:
control moment;
vibration;
micro vibration;
transmission ... See more keywords