Abstract
This paper presents the single-axis angular motion equations of a large space structure assembled in orbit from separate elastic construction elements. We introduce a method to calculate the parameters of discretely varying dynamical properties of an assembled structure whose model has variable coefficients and inherent attributes of an elastic multi-frequency vibrating system. In addition, we suggest a parametrically tuneable algorithm for powered gyro control of such objects that guarantees desired dynamics at all steps of robotized assembly. Simulation results demonstrate the efficiency of the suggested algorithm.
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Original Russian Text © V.M. Glumov, I.N. Krutova, V.M. Sukhanov, 2016, published in Problemy Upravleniya, 2016, No. 1, pp. 82–89.
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Glumov, V.M., Krutova, I.N. & Sukhanov, V.M. Some Features of Powered Gyrostabilization of a Large Space Structure Assembled in Orbit. Autom Remote Control 79, 524–534 (2018). https://doi.org/10.1134/S0005117918030104
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DOI: https://doi.org/10.1134/S0005117918030104