Analysis of dynamic characteristics of flywheel clusters in a spacecraft attitude system

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The results of a comparative analysis of the dynamic characteristics for minimally redundant clusters of flywheels with respect to the variation domaines for the vectors of their angular momentums and control torques, both in the standard configuration and in case of failure of any one flywheel in their composition, are presented.

Spacecraft, attitude control, flywheel clusters, comparison of characteristics

Короткий адрес: https://sciup.org/148323599

IDR: 148323599   |   DOI: 10.37313/1990-5378-2021-23-6-119-125

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