AbstractUtilization of a data-relay satellite (DRS) to obtain range and range-rate measurements of a low Earth-orbiting satellite presents obvious visibility advantages compared to Ground stations. A feasibility study of the orbital estimation of a low-orbiting satellite by means of a Kalman filtering algorithm using DRS measurements has been performed, leading to positive conclusions. The estimation of a launcher ascent trajectory has been also investigated, but no definite conclusions could be stated to date.


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    Titel :

    Satellite and launcher trajectory estimation using a data-relay satellite


    Beteiligte:
    Boissieres, J. (Autor:in)

    Erschienen in:

    Acta Astronautica ; 12 , 7-8 ; 619-627


    Erscheinungsdatum :

    1985-02-16


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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