2015 IEEE Avionics and Vehicle Fiber-Optics and Photonics Conference (AVFOP) 2015
DOI: 10.1109/avfop.2015.7356646
|View full text |Cite
|
Sign up to set email alerts
|

Fiber-optic sensing system: Overview, development and deployment in flight at NASA

Abstract: An overview of the research and technological development of the fiber-optic sensing system (FOSS) at the National Aeronautics and Space Administration Armstrong Flight Research Center (NASA AFRC) is presented. Theory behind fiber Bragg grating (FBG) sensors, as well as interrogation technique based on optical frequency domain reflectometry (OFDR) is discussed. Assessment and validation of FOSS as an accurate measurement tool for structural health monitoring is realized in the laboratory environment as well as… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1

Citation Types

0
3
0

Year Published

2017
2017
2023
2023

Publication Types

Select...
4
1

Relationship

0
5

Authors

Journals

citations
Cited by 7 publications
(3 citation statements)
references
References 1 publication
(1 reference statement)
0
3
0
Order By: Relevance
“…The interdigital electrode is designed as a piezoresistive sensor for improved integration and sensitivity, which is further enhanced using a micro-structured piezoresistive film that covers the interdigital electrode (as shown in fig. S1A) (39). The piezoresistive sensor exhibits an extremely high initial resistance (>100 megohm) and a low resistance (8 kilohm) under 600-kPa pressure (as depicted in fig.…”
Section: Design and Performance Of The Pressure Tsmmentioning
confidence: 99%
See 1 more Smart Citation
“…The interdigital electrode is designed as a piezoresistive sensor for improved integration and sensitivity, which is further enhanced using a micro-structured piezoresistive film that covers the interdigital electrode (as shown in fig. S1A) (39). The piezoresistive sensor exhibits an extremely high initial resistance (>100 megohm) and a low resistance (8 kilohm) under 600-kPa pressure (as depicted in fig.…”
Section: Design and Performance Of The Pressure Tsmmentioning
confidence: 99%
“…The accurate measurement of wing position, displacement, and deformation during flight and its response to wing gusts and atmospheric turbulence is critical for wing shape control and to avoid loss of flight control (45). The fiber optic sensing system (FOSS) developed by NASA (39,42) has shown great potential in wing monitoring due to its lightweight, ease of installation, and dense measurement points. The working principle of FOSS can be found in text S2.…”
Section: Airplane Wing Strain Monitoring Using the Strain Tsmmentioning
confidence: 99%
“…Optical fibers have attracted tremendous attention ever since the first successful fiber manufacturing process was demonstrated in the 1970s. With its advantage of exhibiting high sensitivities to external physical C such as temperature, strain, acoustic vibration, current, pressure, etc., and low transmission losses support remote sensing with minimal signal degradation, it is used in many fields as a sensor [1][2][3]. Optical fiber sensors can be divided into pointwise sensors and distributed sensing in the application.…”
Section: Introductionmentioning
confidence: 99%