Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Prediction of Re-Entry of Space Debris Objects: Constant Gain Kalman Filter Approach


    Beteiligte:
    Anilkumar, A (Autor:in) / Ananthasayanam, M (Autor:in) / SubbaRao, P (Autor:in)

    Kongress:

    AIAA Atmospheric Flight Mechanics Conference and Exhibit



    Erscheinungsdatum :

    01.01.2003




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    AIAA-2003-5393 Prediction of Re-Entry of Space Debris Objects: Constant Gain Kalman Filter Approach

    Ananthasayanam, M. / SubbaRao, P. / Anilkumar, A. et al. | British Library Conference Proceedings | 2003



    Evolution and Expansion of the Orbital Debris Scenario based on Constant Gain Kalman Filter Approach

    Ananthasayanam, M. R. / Anilkumar, A. K. / Subba Rao, P. V. | AIAA | 2004


    Evolution and Expansion of the Orbital Debris Scenario based on Constant Gain Kalman Filter Approach (IAC-04-IAA.5.12.1.10)

    Ananthasayanam, M. R. / Anilkumar, A. K. / Rao, P. V. S. et al. | British Library Conference Proceedings | 2005


    Re-entry of space debris : Proceedings

    Flury, W. ;Longdon, N. | TIBKAT | 1986