Abstract A satellite equipped with a magnetic attitude control system and a pitch flywheel has been considered. The system performance in the transient mode has been investigated. The characteristic exponent of the system have been approximated for a satellite on a circumpolar orbit. In the steady-state mode of gravitational attitude, small motions are considered in the vicinity of equilibrium. The attitude accuracy has been analyzed. The algorithm of an arbitrary but given attitude of the satellite in the orbital plane has been investigated. A numerical simulation has been performed.


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    Titel :

    Motion of a satellite equipped with a pitch flywheel and magnetic coils in gravitational field


    Beteiligte:
    Ovchinnikov, M. Yu. (Autor:in) / Roldugin, D. S. (Autor:in) / Penkov, V. I. (Autor:in) / Varatarao, R. (Autor:in) / Ryabikov, V. S. (Autor:in)

    Erschienen in:

    Cosmic Research ; 55 , 3 ; 207-213


    Erscheinungsdatum :

    2017-05-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Motion of a satellite equipped with a pitch flywheel and magnetic coils in gravitational field

    Ovchinnikov, M. Yu. / Roldugin, D. S. / Penkov, V. I. et al. | Online Contents | 2017


    Erratum to: “Motion of a satellite equipped with a pitch flywheel and magnetic coils in gravitational field”

    Ovchinnikov, M. Yu. / Roldugin, D. S. / Penkov, V. I. et al. | Online Contents | 2017


    Erratum to: “Motion of a satellite equipped with a pitch flywheel and magnetic coils in gravitational field”

    Ovchinnikov, M. Yu. / Roldugin, D. S. / Penkov, V. I. et al. | Springer Verlag | 2017

    Freier Zugriff

    Satellite Flywheel Final Report

    L. D. Barwell / J. Swain | NTIS | 1970


    Flywheel components for satellite applications

    Millner, A.R. | Tema Archiv | 1978