Abstract A satellite with electrodynamic stabilization system is considered. Based on the method of Lyapunov functions, sufficient conditions of the asymptotic stability of direct equilibrium position of this satellite in the orbital coordinate system under perturbing action of a gravitational moment are obtained. These conditions allow one to ensure a rational choice of parametric control coefficients depending on parameters of the satellite and its orbit.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Electrodynamic stabilization of earth-orbiting satellites in equatorial orbits


    Beteiligte:

    Erschienen in:

    Cosmic Research ; 50 , 4 ; 313-318


    Erscheinungsdatum :

    01.07.2012


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Electrodynamic stabilization of earth-orbiting satellites in equatorial orbits

    Aleksandrov, A. Yu. / Tikhonov, A. A. | Online Contents | 2012




    Investigation of electrodynamic stabilization and control of long orbiting tethers

    Colombo, G. / Grossi, M. D. / Dobrowolny, M. et al. | NTRS | 1980


    Robotic Servicing on Earth Orbiting Satellites

    United States; National Aeronautics and Space Administration / United States; Air Force / University of Houston-Clear Lake | British Library Conference Proceedings | 1992