Development of a tool that predicts the orbital parameters of a satellite from an initial state vector for a specified time interval is addressed. The elements used in the algorithm are presented. The prediction performance of the algorithm is demonstrated by using the two line elements of a GPS satellite and the CHAMP scientific satellite.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Development of a Tool for Prediction of the Orbital Parameters of Earth Observation Satellites


    Beteiligte:
    Altay, Alkan (Autor:in) / Karsli, Gizem (Autor:in) / Ozkan, Ahmet (Autor:in)


    Erscheinungsdatum :

    2007-06-01


    Format / Umfang :

    2515927 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Orbital parameters for artificial earth satellites up to 40,000 km altitude

    Catalfamo, C. R. / Harlin, S. H. / Stafford, W. H. | NTRS | 1963


    Threats awaiting Earth observation satellites

    Bodemann, Christian / Kalden, Osman | IEEE | 2013


    Parachute satellites for earth observation

    Massonnet, Didier | Online Contents | 2008


    Parachute satellites for earth observation

    Massonnet, Didier | Elsevier | 2008