DocumentCode :
1021753
Title :
Ensuring GPS navigation integrity using receiver autonomous integrity monitoring
Author :
Michalson, William R.
Author_Institution :
Dept. of Electr. & Comput. Eng., Worcester Polytech. Inst., MA, USA
Volume :
10
Issue :
10
fYear :
1995
fDate :
10/1/1995 12:00:00 AM
Firstpage :
31
Lastpage :
34
Abstract :
The many advantages of Global Positioning System (GPS) based navigation have created a tremendous amount of interest in using GPS as the primary navigation aid onboard commercial and civil aircraft. Even in the presence of Selective Availability, the accuracy of GPS is sufficient to guide aircraft point-to-point between airports without requiring other navigation aids such as VOR or DME. Unfortunately, there is a finite probability that a GPS satellite will fail, causing the transmission of potentially misleading navigation information. Thus, before GPS can be widely adopted as a navigation aid, techniques must be devised to detect any possible failures and notify the user prior to the degradation of navigation accuracy. This paper discusses the problem of detecting possible GPS satellite failures using a technique called Receiver Autonomous Integrity Monitoring (RAIM)
Keywords :
Global Positioning System; aircraft instrumentation; aircraft navigation; GPS navigation integrity; aircraft; navigation accuracy; navigation information; primary navigation aid; receiver autonomous integrity monitoring; Aircraft navigation; Aircraft propulsion; Availability; Clocks; Computerized monitoring; Degradation; Earth; Equations; Global Positioning System; Satellite navigation systems;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE
Publisher :
ieee
ISSN :
0885-8985
Type :
jour
DOI :
10.1109/62.469796
Filename :
469796
Link To Document :
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