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Research on dynamic balancing for large-inertia and complex-shaped satellite payload module in vacuum

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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Published online on

Abstract

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Ahead of Print.
The uneven mass distribution in the satellite payload module causes centrifugal force and torque during its rotation, which significantly affects the on-orbit attitude stability of the satellite and must be controlled. Due to the complex shape and large ...