AbstractThe MiniSTEP drag-free control system must reduce the atmospheric drag forces acting on the spacecraft by seven orders of magnitude, to yield an average residual acceleration of less than 3·10−14 m s−2 averaged over the measurement bandwidth. The origins of the drag-free requirements are discussed, and a control system is presented which meets the requirements under realistic assumptions for noise levels.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The MiniSTEP drag-free control system


    Beteiligte:
    Jafry, Y.R. (Autor:in)

    Erschienen in:

    Advances in Space Research ; 32 , 7 ; 1383-1386


    Erscheinungsdatum :

    2003-01-01


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    The MiniSTEP drag-free control system

    Jafry, Y.R. | Online Contents | 2003


    MiniSTEP

    Vitale, S. | British Library Online Contents | 1997


    The NASA-ESA MiniSTEP payload

    Worden, P.W. | Online Contents | 2003


    The NASA-ESA MiniSTEP project

    Swanson, P.N. | Online Contents | 2003


    Capacitive Sensing and Electrostatic Positioning of the Ministep Test Masses

    Touboul, P. / Foulon, B. / Josselin, V. et al. | British Library Conference Proceedings | 2000