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.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    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:

    Cosmic Research ; 57 , 4 ; 272-288


    Erscheinungsdatum :

    2019-07-01


    Format / Umfang :

    17 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    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. | Online Contents | 2019


    Nanosatellite Launch Adapter System (NLAS)

    Yost, Bruce D. / Hines, John W. / Agasid, Elwood F. et al. | NTRS | 2010


    Nanosatellite Launch Adapter System (NLAS)

    B. D. Yost / J. W. Hines / E. F. Agasid et al. | NTIS | 2010


    Nanosatellite Cluster Launch Collision Analysis

    Santoni, F. | Online Contents | 2013


    ELaNa: Education Launch of Nanosatellite

    Skrobot, Garrett | NTRS | 2011