Modeling of a nanosatellite angular motion damping using hysteresis plate
Matematičeskoe modelirovanie, Tome 32 (2020) no. 2, pp. 101-112

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Mathematical modeling of the angular motion of a CubeSat type nanosatellite with a passive magnetic attitude control system is carried out. 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 hysteresis dampers are studied using laboratory facility. A comparative analysis of the damping time using the plate and a set of rods is presented.
Keywords: nanosatellite, hysteresis damper, angular motion.
@article{MM_2020_32_2_a5,
     author = {D. S. Ivanov and M. Yu. Ovchinnikov and V. I. Penkov and T. A. Ivanova},
     title = {Modeling of a nanosatellite angular motion damping using hysteresis plate},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {101--112},
     publisher = {mathdoc},
     volume = {32},
     number = {2},
     year = {2020},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2020_32_2_a5/}
}
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D. S. Ivanov; M. Yu. Ovchinnikov; V. I. Penkov; T. A. Ivanova. Modeling of a nanosatellite angular motion damping using hysteresis plate. Matematičeskoe modelirovanie, Tome 32 (2020) no. 2, pp. 101-112. http://geodesic.mathdoc.fr/item/MM_2020_32_2_a5/