Journal of Advanced Navigation Technology (한국항행학회논문지)

The Korean Navigation Institute (한국항행학회)
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Abnormal Detection of CTLS Aircraft Wing Structure using SWT

SWT를 이용한 CTLS항공기 날개 구조물 이상탐지

  • 신현성 (한서대학교 대학원 항공시스템공학과) ;
  • 홍교영 (한서대학교 항공전자공학과)
  • Received : 2018.08.28
  • Accepted : 2018.10.23
  • Published : 2018.10.31
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Abstract

In this paper, the noise is removed by using CTLS aircraft installed FBG sensor inside the aircraft wing. We suggest a normal wavelet transform scheme with motion - invariant characteristics for noise reduction. In the case of installing FBG sensors inside the composite material as in CTLS, large and small empty spaces and parts or sections are generated between the adhesive layers, and a signal splitting problem occurs. FBG sensor is not affected by noise. but eletromagnetic, light source, light detector and signal processing device are influeced by noise because these are eletronic components what affected by eletromagnetic wave. because of this, errors are occured. Experimental results show that the noise can be removed using normal wavelet transform and more accurate data detection is possible.

본 논문은 FBG센서를 항공기 날개 내부에 설치한 CTLS항공기를 이용하여 데이터를 받아 잡음제거를 수행하였다. 잡음제거를 위하여 이동불변의 특성을 지닌 정상 웨이블릿 변환 기법을 제시하였다. CTLS와 같이 복합재 내부에 FBG센서를 설치하게 될 경우 접착제 층 사이에 크고 작은 빈공간과 미 접착부분이 생기게 되고, 신호갈라짐 (split problem) 현상이 발생하게 된다. FBG센서 자체가 전자기적 잡음에 영향을 받지 않지만 광원이나 광 검출기, 신호처리장치의 경우 전원을 사용하는 전자부품이기 때문에 이러한 전자기파의 영향을 받아 오차가 발생하게 된다. 이렇게 발생한 오차를 실험결과를 통하여 정상 웨이블릿 변환을 이용하여 잡음을 제거하고 보다 정확한 데이터 검출을 할 수 있음을 확인하였다.

Keywords

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