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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Contributors:

    Publication date :

    1985-07-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


    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


    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



    Low earth orbit constellations: orbit control or not

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