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Modeling a Nanosatellite’s Angular Motion Damping Using a Hysteresis Plate

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Mathematical Models and Computer Simulations Aims and scope

Abstract

The angular motion of a CubeSat-type nanosatellite with a passive magnetic attitude control system is mathematically modelled. The attitude control system consists of a permanent magnet and hysteresis dampers in the form of a plate or a set of rods. The parameters of the hysteresis dampers are studied using a laboratory facility. A comparative analysis of the damping time using the plate and the set of rods is presented.

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Authors and Affiliations

  1. Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, 125047, Moscow, Russia

    D. S. Ivanov, M. Yu. Ovchinnikov & V. I. Penkov

  2. People’s Friendship University, 117198, Moscow, Russia

    T. A. Ivanova

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  1. D. S. Ivanov
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  2. M. Yu. Ovchinnikov
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  3. V. I. Penkov
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  4. T. A. Ivanova
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Correspondence to D. S. Ivanov.

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Ivanov, D.S., Ovchinnikov, M.Y., Penkov, V.I. et al. Modeling a Nanosatellite’s Angular Motion Damping Using a Hysteresis Plate. Math Models Comput Simul 12, 816–823 (2020). https://doi.org/10.1134/S2070048220050075

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  • DOI: https://doi.org/10.1134/S2070048220050075

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