• DocumentCode
    3448256
  • Title

    Design tools for GNSS

  • Author

    Ashkenazi, V. ; Chen, W. ; Ochieng, W.Y. ; Hill, C.J. ; Moore, T.

  • Author_Institution
    Inst. of Eng. Surveying & Space Geodesy, Nottingham Univ., UK
  • fYear
    1995
  • fDate
    35019
  • Firstpage
    42401
  • Lastpage
    42408
  • Abstract
    The process of GNSS constellation design can be divided into two parts. Firstly, it is possible to design a new configuration of satellites, given specific criteria which it must satisfy. Secondly, it is possible to analyse a given constellation, either resulting from the design process, or based on current satellites, to assess the degree to which it meets the specified requirements. A thorough description of the basic theoretical principles of the design of optimal satellite orbits, in terms of satellite availability, coverage, accuracy and integrity, as implemented in the IESSG design software, is given in this paper. As a demonstration of the analysis principles, a number of GNSS constellations have been tested. GNSSI is represented by the two scenarios of GPS plus augmentations
  • Keywords
    Global Positioning System; optimisation; GNSS constellation design; GNSSI; GPS; IESSG design software; accuracy; configuration of satellites; coverage; integrity monitoring; navigation; optimal satellite orbits; satellite availability;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    Implementation of GNSS, IEE Colloquium on
  • Conference_Location
    London
  • Type

    conf

  • DOI
    10.1049/ic:19951306
  • Filename
    494805