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Spacecraft Segment Damage Identification Method Based on Fiber Optic Strain Difference Field Reconstruction and Norm Calculation.
Sensors (Basel). 2023 Oct 30;23(21):8822. doi: 10.3390/s23218822.
Sensors (Basel). 2023.
PMID: 37960522
Free PMC article.
Morphological Reconstruction for Variable Wing Leading Edge Based on the Node Curvature Vectors.
Zeng J, Zhu Q, Zhao Y, Wang Z, Yang Y, Wu Q, Cui J.
Zeng J, et al.
Biomimetics (Basel). 2024 Apr 20;9(4):250. doi: 10.3390/biomimetics9040250.
Biomimetics (Basel). 2024.
PMID: 38667260
Free PMC article.
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