Transient Attitude Motion of TNS-0#2 Nanosatellite during Atmosphere Re-Entry

نویسندگان

چکیده

Attitude motion reconstruction of the Technological NanoSatellite TNS-0 #2 during last month its mission is presented in paper. The satellite was designed to test performance data transmission via Globalstar communication system. This system successfully provided telemetry (even atmosphere re-entry) up an altitude 156 km. Satellite attitude for this phase analyzed nominal represents passive stabilization along a geomagnetic field induction vector. equipped with permanent magnet and hysteresis dampers. axis tracked local direction accuracy about 15 degrees almost two years mission. Rapid decay operation resulted transition from magnetic aerodynamic satellite. details initial tumbling after launch, stabilization, prior subsequent mode are presented.

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ژورنال

عنوان ژورنال: Applied sciences

سال: 2021

ISSN: ['2076-3417']

DOI: https://doi.org/10.3390/app11156784