This paper continues the study of the problem on determination of parameters of the spherical motion of a spacecraft and control of this motion using only the Earth magnetic field. The problem of damping the angular velocity of this spacecraft and construction of three-axis orientation regime is solved. An algorithm for estimation of parameters of the spherical motion, which has a wide region of convergence, is proposed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Control of the spherical motion of a spacecraft in the Earth magnetic field. II. Orientation and stabilization


    Beteiligte:
    Lrbedev, D.V. (Autor:in) / Tkachenko, A.I. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1998


    Format / Umfang :

    3 Seiten, 17 Quellen



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch






    Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control

    Chabot, Joshua / Schaub, Hanspeter | AIAA | 2016


    Solar Pressure Attitude Stabilization of Earth-Pointing Spacecraft

    Pande, K.C. / Venkatachalam, R. | IEEE | 1981


    METHOD FOR DYNAMIC HIGH-ACCURACY ORIENTATION AND STABILIZATION OF SPACECRAFT

    GLUKHOV VITALIJ IVANOVICH / KOVALENKO SERGEJ YUREVICH / MAKEICH SERGEJ GRIGOREVICH et al. | Europäisches Patentamt | 2019

    Freier Zugriff