• DocumentCode
    55741
  • Title

    System using hybrid LEO-GPS satellites for rapid resolution of integer cycle ambiguities

  • Author

    Shiwei Tian ; Weiheng Dai ; Renfu Liu ; Jiang Chang ; Guangxia Li

  • Author_Institution
    Coll. of Commun. Eng., PLA Univ. of Sci. & Technol., Nanjing, China
  • Volume
    50
  • Issue
    3
  • fYear
    2014
  • fDate
    Jul-14
  • Firstpage
    1774
  • Lastpage
    1785
  • Abstract
    Resolution of integer cycle ambiguities is a critical requirement for centimeter-level carrier-phase positioning. This paper investigates the issue of GPS rapid resolution of integer cycle ambiguities, where a Low Earth orbit (LEO) ranging satellite is utilized to obtain large satellite geometry variations generated by its fast-moving property. We define a new system by adding the LEO ranging satellite transmitting signals on the L1 and/or L2 band to the GPS to improve the ability to estimate the integer cycle ambiguities rapidly, and analyse the performance using canonical metrics, such as gain in baseline precision, ambiguity precision and correlation, and ambiguity dilution of precision. Furthermore, in terms of success probability, we evaluate the performance of the proposed scheme compared with that of GPS. In addition, the impacts of the altitude of LEO satellite orbit, the number of visible satellites, the LEO satellite´s L2 navigation frequency, and different locations of the receivers on the ambiguity resolution are further analysed. The performance of the proposed scheme is demonstrated through in-depth numerical simulations.
  • Keywords
    Global Positioning System; correlation methods; numerical analysis; GPS rapid resolution; ambiguity correlation; ambiguity precision; baseline precision; canonical metrics; centimeter-level carrier-phase positioning; hybrid LEO-GPS satellites; in-depth numerical simulations; integer cycle ambiguity; low Earth orbit ranging satellite; navigation frequency; satellite geometry variations; visible satellites; Distance measurement; Geometry; Global Positioning System; Low earth orbit satellites; Mathematical model;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2014.120662
  • Filename
    6965738