Calibration of a Load Measurement System for an Unmanned Aircraft Composite Wing Based on Fibre Bragg Gratings and Electrical Strain Gauges

Calibration of a Load Measurement System for an Unmanned Aircraft Composite Wing Based on Fibre Bragg Gratings and Electrical Strain Gauges

This paper presents the issues concerning calibration of a measurement system for monitoring the cross-sectional forces and moments of an unmanned aircraft’s wing. A composite cantilever wing with built-in measurement systems based on electrical resistance and Fibre Bragg Grating strain ga...

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Bibliographic Details
Main Author: Łukasz Święch
Format: Article
Language:English
Published: MDPI AG 2020-03-01
Series:Aerospace
Subjects:
experimental tests
unmanned aircraft systems
thin-walled composite structures
load monitoring system
fbg strain gauge measurements
electrical resistance strain gauge measurements
Online Access:https://www.mdpi.com/2226-4310/7/3/27

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https://www.mdpi.com/2226-4310/7/3/27

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