Composites Research

The Korean Society for Composite Materials (한국복합재료학회)
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A Study on the Prediction of the Loaded Location of the Composite Laminated Shell by Using Neural Networks

신경회로망을 이용한 복합재료 원통쉘의 하중특성 추론에 관한 연구

  • Published : 2001.10.01
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Abstract

After impact analysis of the composite cylindrical shells was performed. obtained outputs at 9 equally divided points of the shell were used as input patterns of the neural networks. Identification of impact loading characteristics was predicted simultaneously. Momentum backpropagation algorithm of neural networks which can modify the momentum coefficient and learning rate was developed and applied to identify the loading characteristics. Hidden layers of the backpropagation increased from 1 layer to 3 layers and trained the loading characteristics. Developed program with variable learning rate was converged close to real load characteristics under 1% error. Inverse engineering which identify the impact loading characteristics can be applicable to the composite laminated cylindrical shells with developed neural networks.

본 연구에서는 복합재료 원통쉘의 구조해석을 통하여 구해진 원통쉘 경사면의 10등분 등간격 9지점의 변형율을 신경회로망의 입력패턴으로 활용하여 원통쉘에 가해진 중격하중 특성을 동시에 추론하였다. 적용된 신경회로망은 Momentum Backpropagation 알고리즘이며, 모멘텀 계수 및 학습율이 학습도에 따라 가변적으로 조정될 수 있도록 프로그램을 개발 적용하였다 Backpropagation 신경회로망의 은닉층은 1층에서 3층까지 별도 프로그램을 개발하여 충격하중 특성추론 학습을 시도하였다. 개발된 신경회로망 프로그램을 적용하여 원통쉘의 충격하중 특성추론 정확도는 1%이내로 학습에 성공하였다. 본 연구 결과 신경회로망을 이용한 복합재료 원통쉘의 충격하중 특성을 추론할 수 있는 역문제 해석이 가능해졌다.

Keywords

References

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