Reformulation of FRVF with enhanced input stacking for non-square MIMO modal identification of aeronautical structures, validated numerically on a beam and experimentally on Hawk T1A GVT data with performance comparable to existing methods.
Experimental modal analysis of structural systems by using the fast relaxed vector fitting method
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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.
citing papers explorer
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Enhanced input stacking for non-square MIMO modal identification of aeronautical structures via Fast and Relaxed Vector Fitting
Reformulation of FRVF with enhanced input stacking for non-square MIMO modal identification of aeronautical structures, validated numerically on a beam and experimentally on Hawk T1A GVT data with performance comparable to existing methods.
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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.