Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

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


    Beteiligte:

    Kongress:

    55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law ; 2004 ; Vancouver , British Columbia , Canada



    Erscheinungsdatum :

    01.01.2004



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    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


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

    Anilkumar, A / Ananthasayanam, M / SubbaRao, P | AIAA | 2003


    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



    New Approach for the Evolution and Expansion of Space Debris Scenario

    M. R. Ananthasayanam / A. K. Anilkumar / P. V. Subba Rao | AIAA | 2006