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KIAM Preprint № 118, Moscow, 2017
Authors: Ivanov D. S., Koptev M.D., Ovchinnikov M.Y., Pantsyrnyi O.A., Selivanov A.S., Sergeev A.S., Khromov O.E., Yudanov N.A.
Attitude control system of the TNS-0 №2 nanosatellite
Abstract:
A description of the passive magnetic attitude control system of the TNS-0 №2 nanosatellite is presented. Parameters of a permanent magnet and hysteresis rods are given and their choice is justified. The results of laboratory testing of sensors installed in the satellite are shown.
Keywords:
nanosatellite, attitude control system, magnetometer, sun sensor
Publication language: russian,  pages: 20
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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About authors:
  • Ivanov Danil Sergeevich,  danilivanovs@gmail.com,  orcid.org/0000-0002-8253-7092,  KIAM RAS
  • Koptev Michael Dmitrievich,  inflex95@mail.ru,  ВНИЛ ИИС
  • Ovchinnikov Michael Yurievich,  ovchinni@keldysh.ru,  orcid.org/0000-0003-2377-4490,  KIAM RAS
  • Pantsyrnyi Oleg Aleksandrovich,  pantsyrnyi@mail.ru,  Российские космические системы
  • Selivanov Arnold Sergeevich,  selivanov@spacecorp.ru,  Российские космические системы
  • Sergeev Artem Sergeevich,  Российские космические системы
  • Khromov Oleg Evgen'evich,  Российские космические системы
  • Yudanov Nikolay Anatol'evich,  kolyan2606@mail.ru,  Российские космические системы
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