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Development and Flight Testing of an Adaptable Vehicle Health-Monitoring ArchitectureDevelopment and testing of an adaptable wireless health-monitoring architecture for a vehicle fleet is presented. It has three operational levels: one or more remote data acquisition units located throughout the vehicle; a command and control unit located within the vehicle; and a terminal collection unit to collect analysis results from all vehicles. Each level is capable of performing autonomous analysis with a trained adaptable expert system. The remote data acquisition unit has an eight channel programmable digital interface that allows the user discretion for choosing type of sensors; number of sensors, sensor sampling rate, and sampling duration for each sensor. The architecture provides framework for a tributary analysis. All measurements at the lowest operational level are reduced to provide analysis results necessary to gauge changes from established baselines. These are then collected at the next level to identify any global trends or common features from the prior level. This process is repeated until the results are reduced at the highest operational level. In the framework, only analysis results are forwarded to the next level to reduce telemetry congestion. The system's remote data acquisition hardware and non-analysis software have been flight tested on the NASA Langley B757's main landing gear.
Document ID
20030007779
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Woodard, Stanley E.
(NASA Langley Research Center Hampton, VA United States)
Coffey, Neil C.
(NASA Langley Research Center Hampton, VA United States)
Gonzalez, Guillermo A.
(NASA Langley Research Center Hampton, VA United States)
Woodman, Keith L.
(NASA Langley Research Center Hampton, VA United States)
Weathered, Brenton W.
(NASA Langley Research Center Hampton, VA United States)
Rollins, Courtney H.
(NASA Langley Research Center Hampton, VA United States)
Taylor, B. Douglas
(Swales Aerospace Hampton, VA United States)
Brett, Rube R.
(ZIN Technologies, Inc. Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:212139
L-18250
NASA/TM-2003-212139
Report Number: NAS 1.15:212139
Report Number: L-18250
Report Number: NASA/TM-2003-212139
Funding Number(s)
PROJECT: RTOP 706-61-11-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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