Passive System for the Angular Damping of the SAMSAT-QB50 Nanosattelite
- Авторы: Belokonov I.1, Ivanov D.2, Ovchinnikov M.2, Pen’kov V.2
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Учреждения:
- Samara National Research University
- Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
- Выпуск: Том 58, № 5 (2019)
- Страницы: 774-785
- Раздел: 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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Аннотация
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.
Об авторах
I. Belokonov
Samara National Research University
Email: danilivanovs@gmail.com
Россия, Samara, 443086
D. Ivanov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Автор, ответственный за переписку.
Email: danilivanovs@gmail.com
Россия, Moscow, 125047
M. Ovchinnikov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Email: danilivanovs@gmail.com
Россия, Moscow, 125047
V. Pen’kov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Email: danilivanovs@gmail.com
Россия, Moscow, 125047
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