The deployment maneuver of three axis vertical constellations with elastic tethers is analyzed. The deployment strategy devised previously was improved. Dampers were added to the system. Effective algorithms for damping out the fundamental vibrational modes of the system were implemented. Simulations of a complete deployment and a subsequent station keeping phase of a three mass constellation is shown.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Analytical investigation of the dynamics of tethered constellations in Earth orbit (phase 2)


    Beteiligte:
    Lorenzini, E. (Autor:in) / Arnold, D. A. (Autor:in) / Grossi, M. D. (Autor:in) / Gullahorn, G. E. (Autor:in)

    Erscheinungsdatum :

    01.10.1985


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Analytical investigation of the dynamics of tethered constellations in Earth orbit, phase 2

    Lorenzini, Enrico C. / Gullahorn, Gordon E. / Cosmo, Mario L. et al. | NTRS | 1994


    Analytical investigation of the dynamics of tethered constellations in Earth orbit, phase 2

    Lorenzini, E. C. / Arnold, D. A. / Grossi, M. D. et al. | NTRS | 1986



    Low earth orbit constellations: orbit control or not

    Radzik, J. / Maral, G. / Centre National d'Etudes Spatiales et al. | British Library Conference Proceedings | 1993