Assembly-like FEM updating performs ~95% of solves on subassemblies for 28% lower workload proxy effort with fidelity within 1% of global updating on experimental flexible wing data.
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NExT-FRVF operational modal analysis method validated on numerical beam model and real ISS acceleration data, claiming better performance than NExT-ERA and SSI under noise.
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International Space Station operational modal analysis via iterative pole relocation
NExT-FRVF operational modal analysis method validated on numerical beam model and real ISS acceleration data, claiming better performance than NExT-ERA and SSI under noise.