DocumentCode :
1558917
Title :
Sigma inflation for the local area augmentation of GPS
Author :
Pervan, Boris ; Sayim, Irfan
Author_Institution :
Dept. of Mech. & Aerosp. Eng., Illinois Inst. of Technol., Chicago, IL, USA
Volume :
37
Issue :
4
fYear :
2001
fDate :
10/1/2001 12:00:00 AM
Firstpage :
1301
Lastpage :
1311
Abstract :
The Local Area Augmentation System (LAAS) is the differential satellite navigation architectural standard for civil aircraft precision approach and landing. While the system promises great practical benefit, a number of key technical challenges have been encountered in the definition of the architecture. Perhaps chief among these has been the need to ensure compliance with stringent requirements for navigation Integrity. In this context, this research investigates the sensitivity of integrity risk to statistical uncertainties in the knowledge of reference receiver error standard deviation (σpr_gnd ) and error correlation across the multiple reference receivers to be used in the LAAS ground segment. A new, detailed approach toward mitigating the integrity risk due to parameter statistical uncertainty is presented
Keywords :
Gaussian processes; Global Positioning System; aircraft landing guidance; errors; ground support equipment; probability; radio receivers; sensitivity analysis; standards; statistical analysis; LAAS ground segment; civil aircraft; compliance; differential satellite navigation; error correlation; integrity risk; local area augmentation; navigation integrity; precision approach; precision landing; reference receiver error standard deviation; sigma sensitivity analysis; standard; statistical uncertainties; Aerospace electronics; Aerospace engineering; Aircraft navigation; Error correction; Global Positioning System; Monitoring; Protection; Satellite broadcasting; Satellite navigation systems; Uncertainty;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.976966
Filename :
976966
Link To Document :
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