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:
    Cooper, Paul A. (Autor:in) / Stockwell, Alan E. (Autor:in) / Wu, Shih-Chin (Autor:in)

    Kongress:

    MSC World Users'' Conference ; 1993 ; Arlington, VA, United States


    Erscheinungsdatum :

    01.12.1993


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Space Station/Orbiter Berthing Dynamics During an Assembly Flight

    P. A. Cooper / A. E. Stockwell / S. Wu | NTIS | 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



    Control/structure interaction during Space Station Freedom-Orbiter berthing

    Hua, Tuyen / Kubiak, E. / Lin, Yeongching et al. | NTRS | 1993