The method of orbit determination using radio interferometer of small-diameter antennas for low-Earth-orbit (LEO) satellites is proposed. In this method, cross correlation phases are measured between received signals by two antennas. From numerical simulations and real observations analyses using a new software we have developed, orbit determination filter (ODEF), it is confirmed that the satellite position and velocity can be estimated with an accuracy of a few tens of meters and a few tens of mm/s for baseline length of 75 m and the altitude of the satellite of 1400 km. In addition, a numerical simulation makes clear that the position error becomes smaller as the baseline length gets longer.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Orbit Determination using Radio Interferometer of Small-Diameter Antennas for LEO Satellites


    Beteiligte:
    Sakamoto, Y. (Autor:in) / Nishio, M. (Autor:in)


    Erscheinungsdatum :

    01.07.2011


    Format / Umfang :

    1479510 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    GNSS Receive Antennas on Satellites for Precision Orbit Determination

    Zackrisson, J. / Ohgren, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011


    An orbit determination approach for small satellites

    Laneve, G. / Curti, F. | British Library Online Contents | 1997


    An orbit determination approach for small satellites

    Laneve, G. / Curti, F. / European Space Agency | British Library Conference Proceedings | 1997


    Antennas for Small Satellites

    Gao, Steven (Shichang) / Clark, Keith / Zackrisson, Jan et al. | Wiley | 2012


    Antennas for small satellites

    FITZ-COY NORMAN G / SHIRVANTE VIVEK / JOHNSON SHAWN et al. | Europäisches Patentamt | 2018

    Freier Zugriff