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This article is cited in 4 scientific papers (total in 4 papers)
Attitude control system of the TNS-0 № 2 nanosatellite
D. S. Ivanov, M. D. Koptev, M. Yu. Ovchinnikov, O. A. Pantsyrnyi, A. S. Selivanov, A. S. Sergeev, O. E. Khromov, N. A. Yudanov
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.
Citation:
D. S. Ivanov, M. D. Koptev, M. Yu. Ovchinnikov, O. A. Pantsyrnyi, A. S. Selivanov, A. S. Sergeev, O. E. Khromov, N. A. Yudanov, “Attitude control system of the TNS-0 № 2 nanosatellite”, Keldysh Institute preprints, 2017, 118, 20 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2334 https://www.mathnet.ru/eng/ipmp/y2017/p118
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