Abstract
Mathematical models for the deployment and adjustment of a large-sized space-based reflector are presented. Optimal control algorithms are developed for the automatic deployment of antenna elements and tuning of a radio-reflecting mesh. The results of numerical modeling are presented, showing the advantage of using the algorithm for correcting the parameters of the control structure in comparison with the classical methods.
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This work was supported by the Russian Foundation for Basic Research (grant 20-08-00646a).
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Translated by E. Seifina
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Kabanov, S.A., Mitin, F.V. Optimization of the Processes of Deployment and Shape Generation for a Transformable Space-Based Reflector. J. Comput. Syst. Sci. Int. 60, 283–302 (2021). https://doi.org/10.1134/S1064230720060052
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DOI: https://doi.org/10.1134/S1064230720060052