DocumentCode :
2579811
Title :
Differential RAIM and relative RAIM for orbit ephemeris fault detection
Author :
Joerger, Mathieu ; Stevanovic, Stefan ; Khanafseh, Samer ; Pervan, Boris
Author_Institution :
Illinois Inst. of Technol., Chicago, IL, USA
fYear :
2012
fDate :
23-26 April 2012
Firstpage :
174
Lastpage :
187
Abstract :
This paper introduces new monitors for the detection of orbit ephemeris faults affecting differential carrier phase measurements in a shipboard aircraft landing application. Two shipboard monitors are first designed. While they provide high detection performance against two targeted fault types, they are ineffective against the other types of orbit ephemeris faults. In response, to protect the user against the entire threat space, a new airborne receiver autonomous integrity monitoring (RAIM) algorithm is developed. This `unified´ RAIM approach (URAIM) exploits both differential RAIM (which is most efficient at airship separation distances larger than 5 nmi) and relative RAIM (which, in contrast, performs better as the aircraft approaches the ship). Performance evaluations demonstrate URAIM´m potential to detect all types of orbit ephemeris faults using a single, unified residual-based RAIM method.
Keywords :
aircraft landing guidance; fault diagnosis; ships; airship separation; differential RAIM; differential carrier phase measurements; orbit ephemeris fault detection; receiver autonomous integrity monitoring; relative RAIM; shipboard aircraft landing application; shipboard monitors; single unified residual-based RAIM method; unified RAIM approach; Antennas; Extraterrestrial measurements; Frequency measurement; Marine vehicles; Phase measurement; Receivers; Vectors; RAIM; fault detection; integrity monitor; orbit ephemeris fault;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Position Location and Navigation Symposium (PLANS), 2012 IEEE/ION
Conference_Location :
Myrtle Beach, SC
ISSN :
2153-358X
Print_ISBN :
978-1-4673-0385-9
Type :
conf
DOI :
10.1109/PLANS.2012.6236879
Filename :
6236879
Link To Document :
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