This Quarterly Report deals with the deployment maneuver of a single-axis, vertical constellation with three masses. A new, easy to handle, computer code that simulates the two-dimensional dynamics of the constellation has been implemented. This computer code is used for designing control laws for the deployment maneuver that minimizes the acceleration level of the low-g platform during the maneuver.


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    Titel :

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


    Beteiligte:
    Lorenzini, E. (Autor:in)

    Erscheinungsdatum :

    01.07.1985


    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. / Arnold, D. A. / Grossi, M. D. et al. | NTRS | 1985


    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