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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
Abstract:
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.
Keywords:
nanosatellite, attitude motion, magnetometer, sun sensor
Publication language: russian,  pages: 27
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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