Hostname: page-component-78c5997874-lj6df Total loading time: 0 Render date: 2024-11-12T02:16:57.805Z Has data issue: false hasContentIssue false
  • English
  • Français

Carrier Phase Relative RAIM Algorithms and Protection Level Derivation

Published online by Cambridge University Press:  23 February 2010

Livio Gratton ,
Mathieu Joerger  and
Boris Pervan
Livio Gratton
Affiliation:
(Illinois Institute of Technology)
Mathieu Joerger
Affiliation:
(Illinois Institute of Technology)
Boris Pervan*
Affiliation:
(Illinois Institute of Technology)
*
(Email: gratliv@iit.edu)
Get access Rights & Permissions [Opens in a new window]

Abstract

The concept of Relative Receiver Autonomous Integrity Monitoring (RRAIM) using time differential carrier phase measurements is investigated in this paper. The precision of carrier phase measurements allows for mitigation of integrity hazards by implementing RRAIM monitors with tight thresholds without significantly affecting continuity. In order to avoid the need for cycle ambiguity resolution, time differences in carrier phase measurements are used as the basis for detection. In this work, we examine RRAIM within the context of the GNSS Evolutionary Architecture Study (GEAS), which explores potential architectures for aircraft navigation utilizing the satellite signals available in the mid-term future with GPS III. The objectives of the GEAS are focused on system implementations providing worldwide coverage to satisfy LPV-200 operations, and potentially beyond. In this work, we study two different GEAS implementations of RRAIM. General formulas are derived for positioning, fault detection, and protection level generation to meet a given set of integrity and continuity requirements.

Keywords

RRAIMGEASGPS III
Type
Research Article
Information
The Journal of Navigation , Volume 63 , Issue 2 , April 2010 , pp. 215 - 231
Copyright
Copyright © The Royal Institute of Navigation 2010

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

[1]Heo, M., Pervan, B., Pullen, S., Gautier, J., Enge, P., Gebre-Egziabher, D., “Autonomous Fault Detection with Carrier Phase DGPS for Shipboard Landing Navigation,” NAVIGATION, Vol. 51, No. 3, Fall 2004.CrossRefGoogle Scholar
[2]Gratton, L. and Pervan, B., “Carrier Phase Airborne and Ground Monitors for Ionospheric Front Detection for Category III LAAS,” Proceedings of the 19th International Technical Meeting of the Satellite Division of the Institute of Navigation (ION GNSS-2006), Fort Worth, TX, September 26–29, 2006.Google Scholar
[3]Walter, T., Enge, P., Blanch, J., and Pervan, B., “Worldwide Vertical Guidance of Aircraft Based on Modernized GPS and New Integrity Augmentations,” Proceedings of the IEEE, Vol. 96, No. 12, December 2008.CrossRefGoogle Scholar
[4]Lee, Y., “A Position Domain Relative RAIM Method,” Proceedings of the IEEE Position, Location, and Navigation Symposium (PLANS 2008), Monterey, CA, May 5–8, 2008.CrossRefGoogle Scholar
[5]RTCA SC159, DO 229D: “Minimum Operational Performance Standards for Global Positioning System/Wide Area Augmentation System Airborne Equipment”, December 13, 2006.Google Scholar