DocumentCode
2106412
Title
Bias detection and its confidence assessment in Global Positioning System signals
Author
Marti, Lukas ; Van Graas, Frank
Author_Institution
Avionics Eng. Center, Ohio Univ., Athens, OH, USA
Volume
3
fYear
2004
fDate
6-13 March 2004
Abstract
The Federal Aviation Administration plans to migrate to a Global Positioning System (GPS) based navigation system for aeronautical use. As with any safety-critical application, any system failure mode, which might lead to misleading information (MI) for the user, needs to be detected at a high level of confidence. However, the failure detection schemes cannot be too conservative in order not to unreasonably decrease the system´s continuity and/or availability. This work focuses on the detection of GPS signal-in-space anomalies. Since the received GPS signal is altered by noise, any signal parameter determination translates into a statistical estimation process. An estimation procedure to analyze the received satellite signal for possible biases is introduced in this paper. Since the statistical behavior of an anomalous signal is unknown, a distribution-independent detection scheme is presented. Further, the algorithm also provides a confidence assessment on the statistical inference. The derived bias detection procedure is corroborated with simulation results.
Keywords
Global Positioning System; estimation theory; failure analysis; Federal Aviation Administration; GPS signal-in-space anomalies; Global Positioning System signals; bias detection; confidence assessment; failure detection schemes; misleading information; navigation system; noise; safety-critical application; signal parameter determination; statistical estimation process; system failure mode; Aerospace electronics; Aircraft navigation; FAA; Global Positioning System; Military aircraft; RF signals; Radio frequency; Satellite broadcasting; Signal detection; Signal processing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2004. Proceedings. 2004 IEEE
ISSN
1095-323X
Print_ISBN
0-7803-8155-6
Type
conf
DOI
10.1109/AERO.2004.1367935
Filename
1367935
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