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Fault detection and exclusion in multisensor navigation systemsIn order for a multisensor navigation system to meet integrity requirements, there must be a way of detecting erroneous measurements, using only data from those measurements. This can be accomplished using a parity space estimation algorithm. Erroneous measurements must then be removed from the position solution; the entire process is called fault detection and exclusion (FDE). A baseline FDE algorithm has been determined, and is capable of working in real time on present affordable hardware.
Document ID
19960002164
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bernath, Gregory N.
(Ohio Univ. Athens, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Publication Information
Publication: NASA. Langley Research Center, FAA(NASA Joint University Program for Air Transportation Research: 1993-1994
Subject Category
Aircraft Communications And Navigation
Accession Number
96N12172
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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