Enviar artigo por via de e-mail Passive System for the Angular Damping of the SAMSAT-QB50 Nanosattelite
- Autores: Belokonov I.1, Ivanov D.2, Ovchinnikov M.2, Pen’kov V.2
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Afiliações:
- Samara National Research University
- Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
- Edição: Volume 58, Nº 5 (2019)
- Páginas: 774-785
- Seção: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/220494
- DOI: https://doi.org/10.1134/S1064230719050046
- ID: 220494
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Resumo
The angular motion of a nanosatellite equipped with a hysteresis damping system is studied. The required number and sizes of hysteresis rods needed to achieve the specified transient time and aerodynamic orientation with a given accuracy are chosen. Laboratory measurements of parameters of the chosen hysteresis rods are presented. The transient time in the case of abnormal launch of the nanosatellite is estimated.
Sobre autores
I. Belokonov
Samara National Research University
Email: danilivanovs@gmail.com
Rússia, Samara, 443086
D. Ivanov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Autor responsável pela correspondência
Email: danilivanovs@gmail.com
Rússia, Moscow, 125047
M. Ovchinnikov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Email: danilivanovs@gmail.com
Rússia, Moscow, 125047
V. Pen’kov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Email: danilivanovs@gmail.com
Rússia, Moscow, 125047
