电邮这篇文章 Passive System for the Angular Damping of the SAMSAT-QB50 Nanosattelite
- 作者: Belokonov I.1, Ivanov D.2, Ovchinnikov M.2, Pen’kov V.2
-
隶属关系:
- Samara National Research University
- Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
- 期: 卷 58, 编号 5 (2019)
- 页面: 774-785
- 栏目: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/220494
- DOI: https://doi.org/10.1134/S1064230719050046
- ID: 220494
如何引用文章
开放存取
##reader.subscriptionAccessGranted##
订阅存取
详细
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.
作者简介
I. Belokonov
Samara National Research University
Email: danilivanovs@gmail.com
俄罗斯联邦, Samara, 443086
D. Ivanov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
编辑信件的主要联系方式.
Email: danilivanovs@gmail.com
俄罗斯联邦, Moscow, 125047
M. Ovchinnikov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Email: danilivanovs@gmail.com
俄罗斯联邦, Moscow, 125047
V. Pen’kov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Email: danilivanovs@gmail.com
俄罗斯联邦, Moscow, 125047
