The objective of the current research is to identify vibration parameters, including frequencies, damping ratio and uncertainty characteristics, of the Hubble Space Telescope from flight data using an advanced system identification technique. The Observer/Kalman Filter Identification (OKID) technique is used to identify the vibration parameters. The OKID was recently developed by the researchers in the Spacecraft Dynamics Branch at NASA Langley Research Center.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Application of the Observer/Kalman Filter Identification (OKID) Technique to Hubble Flight Data


    Beteiligte:
    J. Juang (Autor:in) / L. G. Horta (Autor:in) / W. K. Belvin (Autor:in) / J. Sharkey (Autor:in) / F. H. Bauer (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    An application of the Observer/Kalman Filter Identification (OKID) technique to Hubble flight data

    Juang, Jer-Nan / Horta, Lucas G. / Belvin, W. Keith et al. | NTRS | 1993


    Improvement of observer/Kalman filter identification (OKID) by residual whitening

    PHAN, MINH / HORTA, LUCAS / JUANG, JER-NAN et al. | AIAA | 1992



    Bilinear Observer/Kalman Filter Identification (AAS 14-307)

    Vicario, F. / Phan, M.Q. / Betti, R. et al. | British Library Conference Proceedings | 2014


    Several recursive techniques for observer/Kalman filter system identification from data

    CHEN, CHUNG-WEN / LEE, GORDON / JUANG, JER-NAN | AIAA | 1992