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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,  страниц: 20
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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