NAVIGATION FOR PRECISION APPROACHES : ROBUST INTEGRITY MONITORING USING GPS + GALILEO

This article presents a discussion of an alternative integrity monitoring technique for GPS navigation systems that does not rely on overbounding errors with a protection limit to safely account for the occasional larger than normal errors. The proposed system needs no assumption on the error distribution, using a technique that marries GPS with Galileo. Describes an algorithm developed for this method. Its elements include a method to select satellite subsets with good geometries, a metric to describe the scatter of position estimates, and a rule to determine the error bound or protection level based on the size of scatter. An illustration uses a simple Galileo-like implementation corresponding to 42 satellites arranged as a Walker 42/7/1 constellation. A hypothetical problem is developed, with the basic computational steps. Includes graphs and scatter plots. The approach is found to require richly redundant measurement steps typical of constellations of 40-plus satellites. But to prove the algorithm meets the false alarm and missed detection requirements will require additional simulations with a more representative satellite array.

  • Availability:
  • Supplemental Notes:
    • Page range: pp 16-18, 20-21
  • Corporate Authors:

    Advanstar Communications, Incorporated

    131 West First Street
    Duluth, MN  United States  55802-2065
  • Authors:
    • Misra, P
    • Bednarz, S
  • Publication Date: 2004-4

Language

  • English

Media Info

  • Features: Figures;
  • Pagination: p. 42-49
  • Serial:
    • GPS World
    • Volume: 15
    • Issue Number: 4
    • Publisher: Advanstar Communications, Incorporated
    • ISSN: 1048-5104

Subject/Index Terms

Filing Info

  • Accession Number: 00974317
  • Record Type: Publication
  • Source Agency: UC Berkeley Transportation Library
  • Files: BTRIS, TRIS
  • Created Date: Jun 2 2004 12:00AM