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KIAM Preprint № 126, Moscow, 2017
Authors: Ivanov D. S., Ovchinnikov M.Y., Pantsyrnyi O.A., Selivanov A.S., Fedorov I.O., Khromov O.E., Yudanov N.A.
Attitude motion of the TNS-0 №2 nanosatellite
A passive attitude motion of the TNS-0 №2 nanosatellite is determined using magnetometer and sun sensor measurements. Time of initial angular motion damping is estimated. The accuracy of the magnetic stabilization is studied.
nanosatellite, attitude motion, magnetometer, sun sensor
Publication language: russian,  pages: 27
Research direction:
Theoretical and applied problems of mechanics
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About authors:
  • Ivanov Danil Sergeevich, RAS
  • Ovchinnikov Michael Yurievich, RAS
  • Pantsyrnyi Oleg Aleksandrovich,  ,  Российские космические системы
  • Selivanov Arnold Sergeevich,  ,  Российские космические системы
  • Fedorov Igor Olegovich,  ,  Российские космические системы
  • Khromov Oleg Evgen'evich,  Российские космические системы
  • Yudanov Nikolay Anatol'evich,  ,  Российские космические системы