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A structural health monitoring project for a composite unmanned aerial vehicle wing: overview and evaluation tests: AN SHM PROJECT FOR A COMPOSITE UAV WING
Open accessAbstract
This special issue introduces an applied research project under which a structural health monitoring (SHM) system was developed for a composite unmanned aerial vehicle (UAV). This special issue consists of five articles that present key studies performed by seven groups through the project. This article is the first one that outlines the project overview, developed components, and evaluation tests. The studies of this project focused on developing key components and algorithms that can be applicable to estimate load and detect damage in composite UAV wing structures. After the system architecture was drawn and the operational scenario was defined, an SHM system was specified as a set of sensor-integrated wing, onboard device, and ground station. Through the project, a series of sensor-integrated structures from coupon specimens to composite wings were fabricated, tested, and damage induced. And the onboard device with compact size was developed and used to monitor external load, structural events, and damage in real time. The ground station was also assembled and applied to estimate the severity, size, and location of damage. Finally, the developed hardware components and algorithms were evaluated through a series of tests. Copyright © 2012 John Wiley & Sons, Ltd.
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References 12 · Cited by 13
Research works printed but not linked: 16
- Zaloga, 2011, World Unmanned Aerial Vehicle Systems, Market Profile and Forecast
- DeGarmo M Nelson GM Prospective unmanned aerial vehicle operations in the future national airspace system Proceedings of AIAA 4th Aviation Technology, Integration and Operations Forum 2004 · DOI
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- Jang B-W Lee Y-G Kim J-H Kim Y-Y Kim C-G Real-time impact identification algorithm for composite structures using fiber Bragg grating sensors submitted to this special issue “A Structural Health Monitoring Project for a Composite UAV wing” Structural Control and Health Monitoring 2012 · DOI
- An Y-K Kim MK Sohn H Airplane hot spot monitoring using integrated impedance and guided wave measurements submitted to this special issue “A Structural Health Monitoring Project for a Composite UAV wing” Structural Control and Health Monitoring 2012 · DOI
- Chia CC Jung H-M Lee J-R Park G Composite aircraft debonding visualization by laser ultrasonic scanning excitation and integrated piezoelectric sensing submitted to this special issue “A Structural Health Monitoring Project for a Composite UAV wing” Structural Control and Health Monitoring 2012 · DOI
- Shin H-J Yun C-Y Park G Farinholt KM Lee J-R Park CY Jun S-M Farrar CR Assessing joint integrity of a lug assembly using piezoelectric active-sensors submitted to this special issue “A Structural Health Monitoring Project for a Composite UAV wing” Structural Control and Health Monitoring 2012 · DOI
- Kim YG Kim JH Kim JW Kim JS Park CY Manufacturing process of sensor installation composite wing box Proceedings of 18 th International Conference on Composite Materials, Jeju, Korea 2011
- Lee BW Seo MS Oh HG Park CY Real-time instrument for structural health monitoring Proceedings of 18 th International Conference on Composite Materials, Jeju, Korea 2011
- Park CY Jun S FBG sensor applications to the structural tests of a newly developed external pod for military jet aircraft Proceedings of Structural Health Monitoring 2009 2009
- Lim, 2011, Impedance based damage detection under varying temperature and loading conditions, NDT & E International, 44, 740, 10.1016/j.ndteint.2011.08.003 · DOI
- Park, 2010, Structural damage monitoring of a composite wing using multiple types of sensors, Advanced Materials Research, 123-125, 907, 10.4028/www.scientific.net/AMR.123-125.907 · DOI
- Lee, 2012, Anomalous wave propagation imaging method with adjacent wave subtraction: application to actual damages in composite wing, Optics & Laser Technology, 44, 428, 10.1016/j.optlastec.2011.12.008 · DOI
- Park, 2012, Bird strike event monitoring in a composite UAV wing using high speed optical fiber sensing system, Composites Science and Technology, 72, 498, 10.1016/j.compscitech.2011.12.008 · DOI
Metadata
- Authors
- Park, C. Y., Kim, J. H., & Jun, S.-M.
- Affiliations
- Agency for Defense Development (KR)
- Corresponding author
- Park, Chan Yik
- Venue
- Structural Control and Health Monitoring
- Publisher
- Hindawi Limited
- Published
- 2012-03-29
- Volume
- 19
- Issue
- 7
- Pages
- 567-579
- ISSN
- 1545-2255 (ISSN-L)
- OpenAlex
- W1597230235
- Cited by
- 13
- References
- 12
- Citations by year
- 2026: 2 · 2023: 2 · 2021: 1 · 2019: 1 · 2018: 1 · 2017: 2 · 2014: 3 · 2012: 1
- FWCI
- 3.14
- Type
- journal article
- Language
- en
- Open access
- bronze
- doi.org
- Locations
- Structural Control and Health Monitoring (publishedVersion)
- Topics
- Physical Sciences › Engineering › Civil and Structural Engineering › Structural Health Monitoring Techniques
- Physical Sciences › Engineering › Aerospace Engineering › Aeroelasticity and Vibration Control
- Physical Sciences › Engineering › Mechanics of Materials › Ultrasonics and Acoustic Wave Propagation
- Keywords
- structural health monitoring, UAV wing, damage detection, load calculation, ground station, damage localization, damage severity estimation, real-time structural monitoring
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