RFI estimation from Non-GSO satellites based on two line element assisted equivalent power flux density calculations

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    Abstract

    As a result of out-of-band emissions and spurious emissions from air-borne or space-borne transmitters simulations and analysis methods have been developed. These methods were developed to determine the amount of interference such a transmitter could cause. The method discussed and applied in this paper is the equivalent power flux density (EPFD) method, which is formally described in international telecommunication union (ITU) recommendations. Up until this point this method has been implemented in MATLAB, which can be used for the determination of the amount of data loss in radio telescopes due to the unwanted emissions of the Iridium satellite constellation. In this paper, it is proposed to use the two line elements (TLEs) instead of the licensed Satellite ToolKit in the EPFD calculation. A theoretical case has been implemented, which is adaptable to the user preferences. The flexibility of the algorithm has been improved, while computational time remains in the same order of magnitude.
    Original languageEnglish
    Title of host publication2018 International Symposium on Electromagnetic Compatibility
    PublisherIEEE Electromagnetic Compatibility Society
    Pages17-21
    Number of pages5
    ISBN (Electronic)978-1-4673-9698-1
    ISBN (Print)978-1-4673-9699-8
    DOIs
    Publication statusPublished - 8 Oct 2018
    EventEMC EUROPE 2018: International Symposium on Electromagnetic Compatibility - Beurs van Berlage, Amsterdam, Netherlands
    Duration: 27 Aug 201830 Aug 2018
    https://www.emceurope2018.org/

    Conference

    ConferenceEMC EUROPE 2018
    Abbreviated titleEMC EUROPE
    CountryNetherlands
    CityAmsterdam
    Period27/08/1830/08/18
    Internet address

    Fingerprint

    Transmitters
    Satellites
    Fluxes
    Radio telescopes
    Iridium
    MATLAB
    Telecommunication
    Air

    Cite this

    @inproceedings{fb6668d1b4af4fcd9f61eaa2b31073a1,
    title = "RFI estimation from Non-GSO satellites based on two line element assisted equivalent power flux density calculations",
    abstract = "As a result of out-of-band emissions and spurious emissions from air-borne or space-borne transmitters simulations and analysis methods have been developed. These methods were developed to determine the amount of interference such a transmitter could cause. The method discussed and applied in this paper is the equivalent power flux density (EPFD) method, which is formally described in international telecommunication union (ITU) recommendations. Up until this point this method has been implemented in MATLAB, which can be used for the determination of the amount of data loss in radio telescopes due to the unwanted emissions of the Iridium satellite constellation. In this paper, it is proposed to use the two line elements (TLEs) instead of the licensed Satellite ToolKit in the EPFD calculation. A theoretical case has been implemented, which is adaptable to the user preferences. The flexibility of the algorithm has been improved, while computational time remains in the same order of magnitude.",
    author = "Hartman, {Thomas Hendrikus Franciscus} and Moonen, {Dominicus Johannes Guilielmus} and Frank Leferink",
    year = "2018",
    month = "10",
    day = "8",
    doi = "10.1109/EMCEurope.2018.8485076",
    language = "English",
    isbn = "978-1-4673-9699-8",
    pages = "17--21",
    booktitle = "2018 International Symposium on Electromagnetic Compatibility",
    publisher = "IEEE Electromagnetic Compatibility Society",

    }

    Hartman, THF, Moonen, DJG & Leferink, F 2018, RFI estimation from Non-GSO satellites based on two line element assisted equivalent power flux density calculations. in 2018 International Symposium on Electromagnetic Compatibility. IEEE Electromagnetic Compatibility Society, pp. 17-21, EMC EUROPE 2018, Amsterdam, Netherlands, 27/08/18. https://doi.org/10.1109/EMCEurope.2018.8485076

    RFI estimation from Non-GSO satellites based on two line element assisted equivalent power flux density calculations. / Hartman, Thomas Hendrikus Franciscus; Moonen, Dominicus Johannes Guilielmus; Leferink, Frank.

    2018 International Symposium on Electromagnetic Compatibility. IEEE Electromagnetic Compatibility Society, 2018. p. 17-21.

    Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

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    AU - Hartman, Thomas Hendrikus Franciscus

    AU - Moonen, Dominicus Johannes Guilielmus

    AU - Leferink, Frank

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    N2 - As a result of out-of-band emissions and spurious emissions from air-borne or space-borne transmitters simulations and analysis methods have been developed. These methods were developed to determine the amount of interference such a transmitter could cause. The method discussed and applied in this paper is the equivalent power flux density (EPFD) method, which is formally described in international telecommunication union (ITU) recommendations. Up until this point this method has been implemented in MATLAB, which can be used for the determination of the amount of data loss in radio telescopes due to the unwanted emissions of the Iridium satellite constellation. In this paper, it is proposed to use the two line elements (TLEs) instead of the licensed Satellite ToolKit in the EPFD calculation. A theoretical case has been implemented, which is adaptable to the user preferences. The flexibility of the algorithm has been improved, while computational time remains in the same order of magnitude.

    AB - As a result of out-of-band emissions and spurious emissions from air-borne or space-borne transmitters simulations and analysis methods have been developed. These methods were developed to determine the amount of interference such a transmitter could cause. The method discussed and applied in this paper is the equivalent power flux density (EPFD) method, which is formally described in international telecommunication union (ITU) recommendations. Up until this point this method has been implemented in MATLAB, which can be used for the determination of the amount of data loss in radio telescopes due to the unwanted emissions of the Iridium satellite constellation. In this paper, it is proposed to use the two line elements (TLEs) instead of the licensed Satellite ToolKit in the EPFD calculation. A theoretical case has been implemented, which is adaptable to the user preferences. The flexibility of the algorithm has been improved, while computational time remains in the same order of magnitude.

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