Abstract
The problem of spacecraft attitude control using electromagnetic systems interacting with the Earth’s magnetic field is considered. A set of dimensionless parameters has been formed to investigate the spacecraft orientation regimes based on dynamically similar models. The results of experimental studies of small spacecraft with a magnetic attitude control system can be extrapolated to the in-orbit spacecraft motion control regimes by using the methods of the dimensional and similarity theory.
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Original Russian Text © V.M. Kulkov, A.L. Medvedskii, V.V. Terentyev, S.O. Firsyuk, A.O. Shemyakov, 2017, published in Doklady Akademii Nauk, 2017, Vol. 477, No. 4, pp. 421–424.
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Kulkov, V.M., Medvedskii, A.L., Terentyev, V.V. et al. Modeling the angular motion dynamics of spacecraft with a magnetic attitude control system based on experimental studies and dynamic similarity. Dokl. Phys. 62, 543–546 (2017). https://doi.org/10.1134/S1028335817120011
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DOI: https://doi.org/10.1134/S1028335817120011