Abstract Description of the passive magnetic attitude control system of the TNS-0 # 2 nanosatellite is presented. The parameters of the main components of the attitude control system are given and their choice is justified. Using telemetry data, the passive angular motion of TNS-0 # 2 was determined after processing measurements of the on-board sensors after launching from the ISS on August 17, 2017. The damping time of the initial angular velocity was estimated. The accuracy of magnetic stabilization after the end of transient processes was determined.
Angular Motion of the TNS-0 # 2 Nanosatellite after Launch from the International Space Station
Cosmic Research ; 57 , 4 ; 272-288
2019-07-01
17 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Angular Motion of the TNS-0 # 2 Nanosatellite after Launch from the International Space Station
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