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Fault detection and isolationIn order for a current satellite-based navigation system (such as the Global Positioning System, GPS) to meet integrity requirements, there must be a way of detecting erroneous measurements, without help from outside the system. This process is called Fault Detection and Isolation (FDI). Fault detection requires at least one redundant measurement, and can be done with a parity space algorithm. The best way around the fault isolation problem is not necessarily isolating the bad measurement, but finding a new combination of measurements which excludes it.
Document ID
19940022786
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bernath, Greg
(Ohio Univ. Athens, OH, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1994
Publication Information
Publication: NASA. Langley Research Center, FAA(NASA Joint University Program for Air Transportation Research, 1992-1993
Subject Category
Quality Assurance And Reliability
Accession Number
94N27289
Funding Number(s)
CONTRACT_GRANT: NGR-36-009-17
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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