Attitude control system of the TNS-0 №2 nanosatellite-Reference-Cited by-同舟云学术

Attitude control system of the TNS-0 №2 nanosatellite

Published:2017 Issue:118 Volume: Page:1-20
ISSN:2071-2898
Container-title:Keldysh Institute Preprints
language:
Short-container-title:KIAM Prepr.

Author:

Ivanov Danil Sergeevich¹^ORCID,Koptev Michael Dmitrievich,Ovchinnikov Michael Yurievich¹,Pantsyrnyi Oleg Aleksandrovich,Selivanov Arnold Sergeevich,Sergeev Artem Sergeevich,Khromov Oleg Evgen'evich,Yudanov Nikolay Anatol'evich

Affiliation:

1. Keldysh Institute of Applied Mathematics

Publisher

Keldysh Institute of Applied Mathematics

Subject

General Medicine

Reference9 articles.

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2. Карпенко С.О. и др. Система ориентации первого российского нано-спутника ТНС-0 №1 // Космические исследования. 2010. Т. 48. № 6. С. 532–540.

3. Ovchinnikov M.Y. et al. Attitude dynamics of the first Russian nanosatellite TNS-0 // Acta Astronaut. 2007. V. 61. № 1–6. pp. 277–285.

4. Ильин А.А., Куприянова Н.В., Овчинников М.Ю. Стационарные вращательные движения твердого тела с сильным магнитом в переменном магнитном поле при наличии диссипации // Известия РАН, Серия Механика твердого тела. 2009. № 3. С. 12–24.

5. Овчинников М.Ю. и др. Магнитные системы ориентации малых спутников. М.: ИПМ им.М.В.Келдыша, 2016. 365 c. ISBN 978-5-98354-028-6. DOI: 10.20948/mono-2016-ovchinnikov

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