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.


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    Titel :

    Angular Motion of the TNS-0 # 2 Nanosatellite after Launch from the International Space Station


    Beteiligte:
    Ivanov, D. S. (Autor:in) / Ovchinnikov, M. Yu. (Autor:in) / Pantsyrnyi, O. A. (Autor:in) / Selivanov, A. S. (Autor:in) / Sergeev, A. S. (Autor:in) / Fedorov, I. O. (Autor:in) / Khromov, O. E. (Autor:in) / Yudanov, N. A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2019




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :

    Klassifikation :

    BKL:    55.60 Raumfahrttechnik / 39.00 Astronomie: Allgemeines / 50.93 Weltraumforschung
    Lokalklassifikation TIB:    770/3520/8000



    Angular Motion of the TNS-0 # 2 Nanosatellite after Launch from the International Space Station

    Ivanov, D. S. / Ovchinnikov, M. Yu. / Pantsyrnyi, O. A. et al. | Springer Verlag | 2019


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