Spacecraft Segment Damage Identification Method Based on Fiber Optic Strain Difference Field Reconstruction and Norm Calculation.

Xu, Jihong; Zeng, Jie; Chen, Binbin; Lu, Ruixin; Zhu, Yangyang; Qi, Lei; Chen, Xiangfei

Xu, Jihong; Zeng, Jie; Chen, Binbin; Lu, Ruixin; Zhu, Yangyang; Qi, Lei; Chen, Xiangfei.

Afiliação

Xu J; College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.
Zeng J; College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.
Chen B; College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.
Lu R; College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.
Zhu Y; College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.
Qi L; Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China.
Chen X; College of Engineering and Applied Sciences, Nanjing University, Nanjing 210023, China.

Sensors (Basel) ; 23(21)2023 Oct 30.

Article em En | MEDLINE | ID: mdl-37960522

Palavras-chave

damage recognition; fiber optic grating sensor; spacecraft segment structure; strain response difference field; vector norms

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Texto completo: 1 Coleções: 01-internacional Base de dados: MEDLINE Idioma: En Ano de publicação: 2023 Tipo de documento: Article

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Texto completo: 1 Coleções: 01-internacional Base de dados: MEDLINE Idioma: En Ano de publicação: 2023 Tipo de documento: Article