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Acceleration and Velocity Sensing from Measured StrainA simple approach for computing acceleration and velocity of a structure from the strain is proposed in this study. First, deflection and slope of the structure are computed from the strain using a two-step theory. Frequencies of the structure are computed from the time histories of strain using a parameter estimation technique together with an autoregressive moving average model. From deflection, slope, and frequencies of the structure, acceleration and velocity of the structure can be obtained using the proposed approach. Simple harmonic motion is assumed for the acceleration computations, and the central difference equation with a linear autoregressive model is used for the computations of velocity. A cantilevered rectangular wing model is used to validate the simple approach. Quality of the computed deflection, acceleration, and velocity values are independent of the number of fibers. The central difference equation with a linear autoregressive model proposed in this study follows the target response with reasonable accuracy. Therefore, the handicap of the backward difference equation, phase shift, is successfully overcome.


Document ID
20160000696
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Pak, Chan-Gi
(NASA Dryden Flight Research Center Edwards, CA United States)
Truax, Roger
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
January 12, 2016
Publication Date
November 30, 2015
Subject Category
Aircraft Stability And Control
Aircraft Design, Testing And Performance
Report/Patent Number
DFRC-E-DAA-TN26642
Report Number: DFRC-E-DAA-TN26642
Meeting Information
Meeting: AIAA SciTech 2016
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
shape sensing
system equivalent reduction and expansion process
fiber optic strain sensor
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