Passive System for the Angular Damping of the SAMSAT-QB50 Nanosattelite
- Авторлар: Belokonov I.1, Ivanov D.2, Ovchinnikov M.2, Pen’kov V.2
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Мекемелер:
- Samara National Research University
- Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
- Шығарылым: Том 58, № 5 (2019)
- Беттер: 774-785
- Бөлім: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/220494
- DOI: https://doi.org/10.1134/S1064230719050046
- ID: 220494
Дәйексөз келтіру
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.
Авторлар туралы
I. Belokonov
Samara National Research University
Email: danilivanovs@gmail.com
Ресей, Samara, 443086
D. Ivanov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Хат алмасуға жауапты Автор.
Email: danilivanovs@gmail.com
Ресей, Moscow, 125047
M. Ovchinnikov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Email: danilivanovs@gmail.com
Ресей, Moscow, 125047
V. Pen’kov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Email: danilivanovs@gmail.com
Ресей, Moscow, 125047