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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
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.
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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