항공기 탑재를 위한 FBG 센서 장비의 설계조건 도출Design Scheme of FBG Sensor System for Aircraft Application

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In this research, design scheme of fiber Bragg grating(FBG) sensor system for aircraft application is suggested from the results and the know-how from the fon11er researches on structural health monitoring techniques using fiber optic sensors. Design factors to be taken into consideration were derived for both sensor parts including connection and system parts. For the stability of FBG sensor system, design requirements of temperature, vibration, humidity, electromagnetic interference were presented from U. S. military standards. The direction of software programming which increases stability and perfon11ance of the aircraft with the FBG sensor system was also examined.
Publisher
한국복합재료학회
Issue Date
2005-11-18
Language
KOR
Citation

2005 한국복합재료학회 추계학술대회, pp.215 - 218

URI
http://hdl.handle.net/10203/15689
Appears in Collection
AE-Conference Papers(학술회의논문)
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항공기 탑재를 위한 FBG 센서 장비의 설계조건 도출.pdf(1.04 MB)Download

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