2 research outputs found

    Attitude control system of the TNS-0 â„–2 nanosatellite

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    Abstract: A description of the passive magnetic attitude control system of the TNS-0 â„–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.Note: Research direction:Theoretical and applied problems of mechanic
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