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.

This article is cited 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.

DOI: 10.20948/prepr-2017-118