A large-angle, multi-body, dynamic modeling capability was developed to help validate numerical simulations of the dynamic motion and control forces which occur while berthing Space Station Freedom to the Shuttle Orbiter during early assembly flights. The paper describes the dynamics and control of the station, the attached Shuttle Remote Manipulator System, and the Orbiter during a maneuver from a gravity-gradient attitude to a torque equilibrium attitude using the station reaction control jets. The influence of the elastic behavior of the station and of the remote manipulator system on the attitude control of the station/Orbiter system during the maneuver is investigated. The flexibility of the station and the arm had only a minor influence on the attitude control of the system during the maneuver.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Space Station/Orbiter Berthing Dynamics During an Assembly Flight


    Beteiligte:
    P. A. Cooper (Autor:in) / A. E. Stockwell (Autor:in) / S. Wu (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    22 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Space Station/Orbiter berthing dynamics during an assembly flight

    Cooper, Paul A. / Stockwell, Alan E. / Wu, Shih-Chin | NTRS | 1993


    Space Station ATCS Performance During Orbiter Berthing

    Kantara, James J. / Graf, Jonathan | SAE Technical Papers | 1993


    Space Station Freedom Attitude Control During Orbiter Berthing

    Garrison, J. L. / Montgomery, R. C. / Virginia Polytechnic Institute and State University | British Library Conference Proceedings | 1993