A new method has been developed to design an active vibration isolation system for microgravity space experiments. This method yields the required controller transfer functions for a specified transmissibility. Hence, it is a straightforward task to guarantee that the desired vibration isolation performance is achieved at each frequency. The theory for such a controller design has been presented by considering a single degree of freedom system. The magnitude of the control force required by the new method has been found to be less than that used by a standard phase lead/lag compensator.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A new approach to controller design for microgravity isolation systems


    Beteiligte:
    Sinha, A. (Autor:in) / Kao, C. K. (Autor:in) / Grodsinsky, C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1990-12-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    The microgravity vibration isolation mount: a dynamic model for optimal controller design

    Hampton, R.D. / Tryggvason, B.V. / Decarufel, J. et al. | Tema Archiv | 1997



    Microgravity Isolation System Design: A Case Study

    Hampton, R.D. | Online Contents | 1996


    Microgravity Isolation System Design: A Case Study

    R. David Hampton / Carl R. Knospe / Carlos M. Grodsinsky | AIAA | 1996