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

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. © 2020, Pleiades Publishing, Ltd.

Authors
Ivanov D.S.1 , Ovchinnikov M.Y.1 , Penkov V.I.1 , Ivanova T.A. 2
Journal
Mathematical Models and Computer Simulations
Publisher
Pleiades Publishing
Number of issue
5
Language
English
Pages
816-823
Status
Published
Link
External link
DOI
10.1134/S2070048220050075
Volume
12
Year
2020
Organizations
  • 1 Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Moscow, 125047, Russian Federation
  • 2 People’s Friendship University, Moscow, 117198, Russian Federation
Keywords
angular motion; hysteresis damper; nanosatellite
Date of creation
02.11.2020
Date of change
02.11.2020
Short link
https://repository.rudn.ru/en/records/article/record/64416/
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