Distributed sensing of a cantilever beam and plate using a fiber optic sensing system

Patrick S. Heaney, Thomas G. Ivanco, Onur Bilgen

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Scopus citations

Abstract

As the capabilities of Fiber Optic Sensing Systems continue to improve, their application to real-time distributed sensing for structural analysis and control of flexible systems is becoming increasingly feasible. This paper reports experimental results on the use of a Fiber Optic Sensing System for static and dynamic shape estimation of a cantilever beam and plate. Demonstrating the use of this sensor technology in benchtop experiments is the first step in effectively incorporating fiber optic sensors in the Integrated Adaptive Wing Technology Maturation aeroelastic half-span wind tunnel model for real-time shape sensing and feedback for drag optimization, maneuver load alleviation, gust load alleviation, and flutter suppression control laws. The effectiveness of the sensing system is analyzed and the application of these results to future aeroelastic experimentation is discussed.

Original languageEnglish (US)
Title of host publication2018 Applied Aerodynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105593
DOIs
StatePublished - 2018
Event36th AIAA Applied Aerodynamics Conference, 2018 - [state] GA, United States
Duration: Jun 25 2018Jun 29 2018

Publication series

Name2018 Applied Aerodynamics Conference

Conference

Conference36th AIAA Applied Aerodynamics Conference, 2018
Country/TerritoryUnited States
City[state] GA
Period6/25/186/29/18

ASJC Scopus subject areas

  • Aerospace Engineering
  • Mechanical Engineering

Fingerprint

Dive into the research topics of 'Distributed sensing of a cantilever beam and plate using a fiber optic sensing system'. Together they form a unique fingerprint.

Cite this