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Fiber Optic Sensing System (FOSS) Technology - A New Sensor Paradigm for Comprehensive Structural Monitoring and Model Validation Throughout the Vehicle Life-CycleThis presentation highlights the usefulness of the FOSS measurement capabilities by the operational load estimation method.
Document ID
20160001157
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Pena, Francisco (NASA Dryden Flight Research Center Edwards, CA United States)
Richards, Lance (NASA Dryden Flight Research Center Edwards, CA United States)
Parker, Allen R., Jr. (NASA Dryden Flight Research Center Edwards, CA United States)
Piazza, Anthony (NASA Dryden Flight Research Center Edwards, CA United States)
Chan, Patrick (NASA Dryden Flight Research Center Edwards, CA United States)
Hamory, Phil (NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
January 26, 2016
Publication Date
January 20, 2015
Subject Category
Optics
Report/Patent Number
DFRC-E-DAA-TN29338
Report Number: DFRC-E-DAA-TN29338
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
fiber optics
FOSS
Fiber Grating Bragg

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IDRelationTitle20150023019See AlsoFiber Optic Sensing System Technology (FOSS): A New Sensor Paradigm for Comprehensive Subsystem Model Validation throughout the Vehicle Life-Cycle20150023019See AlsoFiber Optic Sensing System Technology (FOSS): A New Sensor Paradigm for Comprehensive Subsystem Model Validation throughout the Vehicle Life-Cycle
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