Authors: T. A. Dardeno, A. J. Hughes, L. A. Bull, R. S. Mills, N. Dervilis, K. Worden
Organizations: Dynamics Research Group, School of Mechanical, Aerospace and Civil Engineering, University of Sheffield, Sheffield S1 3JD, UK · School of Mathematics and Statistics, University of Glasgow, Glasgow G12 8SQ, Scotland
Despite recent advances in population-based structural health monitoring (PBSHM), knowledge transfer between highly-disparate structures (i.e., heterogeneous populations) remains a challenge. The current work proposes that heterogeneous transfer may be accomplished via intermediate structures that bridge the gap in information between the structures of interest. A key aspect of the technique is the idea that by varying parameters such as material properties and geometry, one structure can be continuously morphed into another. The approach is demonstrated via a case study involving the parameterisation of (and transfer between) simulated heterogeneous bridge designs (Case 1). Transfer between simplified physical representations of a 'bridge' and 'aeroplane' is then demonstrated in Case 2, via a chain of finite-element models. The facetious question 'When is a bridge not an aeroplane?' has been previously asked in the context of predicting positive transfer based on structural similarity. While the obvious answer to this question is 'Always,' the results presented in the current paper show that, in some cases, positive transfer can indeed be achieved between highly-disparate systems.
Figures & tables
Figure 1: Schematic of geometrical model of PBSHM in terms of a fibre bundle.
Figure 2: A geodesic (red curve) on a sphere, with tangent spaces (planes) shown at successive points along the path. The blue arrows show the tangent directions evolving continuously along the geodesic, illustrating the geodesic flow.
Figure 4: Two-span source (a) and three-span target bridges (b) in the damaged state.
Figure 5: Schematic of model generation process. The first support remained fixed while the second support moved to the right and materialised as α increased.
Figure 6: Cosine alignment along the transfer path for Case 1. The alignment between the current source and target is shown in black with × markers, with values close to 1 indicating that adjacent structures in the chain are consistently similar. The alignment between the current source and the original source is shown in black with ∙ markers, with decreasing values showing progressively less similarity as the chain moves farther away from the original source.
Figure 7: Heterogeneous transfer approach via intermediate structures.
Linear
Geodesic Flow Kernel
K
Accuracy (%)
Best chain
Accuracy (%)
Best chain
0
44.44±0.00
(no chain)
46.76±9.51
(no chain)
1
44.70±4.08
[1 10 18]
67.46±25.24
[1 11 18]
2
57.16±22.11
[1 5 13 18]
94.75±15.83
[1 9 13 18]
3
74.03±26.96
[1 4 12 13 18]
98.82±7.57
[1 4 12 13 18]
4
93.59±17.85
[1 8 11 13 14 18]
99.82±3.11
[1 8 11 13 14 18]
Table 2: Best chains per number of intermediates K for linear and GFK classification approaches. Values are mean ± standard deviation over 1000 noise realisations.
Figure 8: Experimental setup for bridge (a) and aeroplane (b) structures.
Figure 9: Damage to the deck (D1) (a) and (b) column (D2).
Figure 10: Lower bending modes for the bridge and aeroplane. Bridge modes at approximately (a) 100 Hz, (b) 116 Hz, and (c) 150 Hz. Aeroplane repeated root modes at approximately 117 Hz (d), (e).
Figure 11: Representative input spectra, coherence, and FRFs for healthy and damaged states for the bridge configuration.
Figure 12: Sensor layout for all analyses. Accelerometers are shown in red, except for the drive point location which is shown in blue. All units are in mm, and measured from the right-hand edge of the deck/wing.
Figure 13: FRFs from a variability study on the bridge, where four different decks, and four different columns, were removed and reinstalled using consistent torque for the bolts.
Structure
Component
L (m)
W (m)
H (m)
E (Pa)
ρ (kg/m 3 )
Bridge
Deck
1.00
0.10
0.010
6.8×1010
2830
Supports
0.0254
0.0254
0.220
↓
↓
Foot pads
0.0762
0.0762
0.010
Aeroplane
Wings
1.00
0.10
0.010
6.8×1010
2830
Supports
0.0254
0.0254
0.220
↓
↓
Foot pads
0.0762
0.0762
0.010
Table 3: Geometry and material properties for the bridge and aeroplane.
Figure 14: FRFs at drive-point location for experimental bridge, subset of FEM intermediates, and experimental aeroplane. The blue, green, and red curves correspond to the healthy, D1, and D2 classes, respectively.
Figure 15: Subset of intermediate geometries (1, 85, 168, 251, 293, 376, 459, and 500). Images are read top-to-bottom in the left column, then top-to-bottom in the right column.
Figure 16: Cosine alignment along the transfer path at each sensor location for Case 2. The alignment between the current source and target is shown in black with × markers, with values close to 1 indicating that adjacent structures in the chain are consistently similar. The alignment between the current source and the original source is shown in black with ∙ markers, with decreasing values showing progressively less similarity as the chain moves farther away from the original source.
Sensor
Linear Kernel (%)
Geodesic Flow Kernel (%)
1
28.57±0.00
60.64±11.90
2
64.29±0.00
64.28±0.05
3
64.29±0.00
64.29±0.00
5
64.29±0.00
67.17±13.74
6
63.92±9.41
63.59±12.51
7
64.29±0.00
61.26±11.89
Table 4: Transfer accuracy at the final hop without intermediates ( K=0 ) for Linear and GFK approaches in Case 2. Values are mean ± standard deviation over 400 noise realisations.
Sensor
Linear Kernel (%)
Geodesic Flow Kernel (%)
1
35.71±0.00
35.71±0.00
2
35.71±0.00
100.00±0.00
3
100.00±0.00
100.00±0.00
5
100.00±0.00
100.00±0.00
6
64.29±0.00
100.00±0.00
7
64.29±0.00
100.00±0.00
Table 5: Transfer accuracy at the final hop for Linear and GFK approaches in Case 2 using K=4 intermediates: 71, 201, 351, and 500. Values are mean ± standard deviation over 25 noise realisations.
Sensor
Linear Kernel (%)
Geodesic Flow Kernel (%)
1
35.71±0.00
35.69±0.38
2
35.71±0.00
52.27±17.82
3
35.71±0.00
36.45±4.53
5
35.71±0.00
35.71±0.00
6
35.71±0.00
40.86±10.99
7
35.71±0.00
48.20±14.19
Table 6: Transfer accuracy at the final hop for Linear and GFK approaches in Case 2 using K=5 intermediates: 71, 201, 251, 351, and 500. Values are mean ± standard deviation over 350 noise realisations.
Sensor
Linear Kernel (%)
Geodesic Flow Kernel (%)
1
64.29±0.00
87.94±16.91
2
35.71±0.00
38.37±4.33
3
100.00±0.00
100.00±0.00
5
100.00±0.00
100.00±0.00
6
100.00±0.00
100.00±0.00
7
57.37±13.86
100.00±0.00
Table 7: Transfer accuracy at the final hop for Linear and GFK approaches in Case 2 using K=9 intermediates: 26, 31, 91, 101, 181, 219, 291, 401, 500. Values are mean ± standard deviation over 385 noise realisations.
Sensor
Linear Kernel (%)
Geodesic Flow Kernel (%)
1
100.00±0.00
100.00±0.00
2
91.71±0.99
100.00±0.00
3
100.00±0.00
100.00±0.00
5
100.00±0.00
100.00±0.00
6
100.00±0.00
100.00±0.00
7
100.00±0.00
100.00±0.00
Table 8: Transfer accuracy at the final hop for Linear and GFK approaches in Case 2 using all intermediates ( K=500 ). Values are mean ± standard deviation over 25 noise realisations.
Figure 17: A subset of the confusion matrices for Case 2 transfer configurations. Top row: Sensor 1, (a) GFK with K=0 (no intermediates) and (b) K=9 . Middle row: Sensor 2, (c) GFK with K=0 and (d) K=5 . Bottom: Sensor 2, (e) Linear with the full chain ( K=500 ). Matrices are averaged over the corresponding noise realisations reported in Tables 4 to 8 .
This paper presents a methodology-centered transfer learning framework for fragility adaptation under domain shift, class imbalance, and scarce target labels while preserving engineering interpretability and supporting decision-making under uncertainty. Four transfer learning strategies (instance-based, parameter-based, hierarchical Bayesian, and multi-source) are demonstrated through three complementary case studies: (i) instance-based transfer learning via importance weighting, demonstrated on coastal bridge fragility using Hurricane Katrina observations; (ii) parameter-based transfer learning together with hierarchical Bayesian transfer learning, enabling partial pooling across strata and posterior uncertainty quantification, demonstrated on residential building fragility using Hurricane Ian observations; and (iii) multi-source transfer learning that fuses multiple analytical fragility models with learned source weights and regularized target-domain adaptation, demonstrated on seismic bridge fragility using observations from the 2001 Nisqually earthquake. Across these case studies, direct transfer of source models (i.e. using existing state-of-the-art models) fails under domain shift and severe class imbalance, while targeted adaptation substantially improves failure detection and predictive stability in low-data regimes. These findings highlight the need for systematic guidance on diagnostics, strategy selection, and uncertainty reporting when developing and adapting fragility models.
Narges Saeednejad, Jamie Ellen Padgett
Department of Civil and Environmental Engineering, Rice University, Houston, TX, USA · Ken Kennedy Institute, Rice University, Houston, TX, USA
Transfer learning is a natural strategy when a target population has limited data but multiple related auxiliary sources are available. A central difficulty is source heterogeneity: auxiliary sources may not be equally useful, and their usefulness may vary in a structured, cluster-like fashion. Existing transfer-learning methods often reduce source selection to a binary informative/non-informative decision, overlooking subgroups of sources with differential transferability. Motivated by a suicide-risk study using data from the Connecticut Hospital Information Management Exchange (CHIME), comprising 636,758 patients across 27 hospitals, we propose Trans-GLMC, a cluster-structured transfer-learning procedure for generalized linear models. The CHIME setting illustrates the core challenge: hospital-specific risk models are unstable because suicide attempts are rare at any single facility, whereas indiscriminate pooling across hospitals can obscure facility-level differences in patient mix and risk profiles. Trans-GLMC first constructs a coefficient-based distance among the target and candidate sources to recover latent source clusters. It then combines global fusion, within-cluster refinement, and target debiasing to produce an estimator that adapts to the detected structure. We establish a non-asymptotic error bound that improves over its unclustered counterpart whenever a meaningful target cluster exists and matches the unclustered rate up to constants otherwise. In simulations and in the CHIME study, Trans-GLMC improves facility-specific prediction, identifies interpretable communities of hospitals with mutual transferability, and recovers clinically coherent suicide-risk factors.
Xiaohui Yin, Jun Jin, Shane J. Sacco +2
Department of Statistics, University of Connecticut · Department of Public Health Sciences, Henry Ford Health · Center for Population Health, University of Connecticut Health Center
A natural strategy for inverse problems with scarce labelled data is to transfer relational structure learned from abundant forward-simulation data. We show this strategy fails systematically, even when it satisfies the standard theoretical justification for why structure should help. We prove that approximate structure provides estimation-error benefits whenever the edge error satisfies Δ<n2−kn, reducing sample complexity from O(n2) to O(kn+Δ). Structure learned via Neural Relational Inference (NRI) from dynamics prediction satisfies this condition, yet on a source-localisation task across 180 CFD-simulated hydrogen-leak scenarios and 180 acoustic scenarios, it degrades performance by 116% and 201% relative to a flexible, task-optimised attention baseline, while a physics-based prior (Green's function) degrades by only 69-72%. Four independent lines of evidence show this is not a tuning failure: NRI improves only 0.5% when given 18x more training data (versus 16.6% for the task-optimised baseline, p<0.001); performance is insensitive to the NRI edge threshold across a wide range; the dynamics-learned graph overlaps the task-optimal graph on only 6% of edges; and two further dynamics-derived structure estimators (correlation- and mutual-information-based) show no measurable benefit over a structure-free baseline, with the correlation-based estimator performing markedly worse. We formalise this gap as a statement about approximation error that the edge-accuracy condition cannot control, and we provide a lightweight transferability test (Jaccard similarity against a partially-observed target-task graph) that separates successful from failed transfer in all four domain/structure pairs we evaluate, using under an hour of computation and 15-20% of target-domain data; we present this as a heuristic calibrated on few cases, not a validated general threshold.
Nicholas Tan Jerome, Fangnian Wang
Institute for Data Processing and Electronics (IPE) Karlsruhe Institute of Technology (KIT) Karlsruhe, Germany · Institute for Thermal Energy Technology and Safety (ITES) Karlsruhe Institute of Technology (KIT) Karlsruhe, Germany