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Natural Excitation Technique and Eigensystem Realization Algorithm for Phase I of the IASC-ASCE Benchmark Problem: Simulated Data
265
Citations
12
References
2003
Year
Numerical AnalysisEngineeringEigensystem Realization AlgorithmStructural DynamicsMechanical EngineeringVibration MeasurementSpectrum EstimationVibration AnalysisStructural EngineeringStructural IdentificationModal AnalysisVibrationsBenchmark StudyNumerical SimulationBenchmark ProblemSystems EngineeringModeling And SimulationComputational ElectromagneticsStructural VibrationComputer EngineeringStructural Health MonitoringSignal ProcessingNatural Excitation TechniqueCivil EngineeringSpectral AnalysisStructural AnalysisIasc-asce Benchmark ProblemVibration Control
The benchmark study was designed to enable comparison of structural health monitoring methods. The study uses simulated acceleration data from an analytical model, adds broadband noise, and applies a natural excitation technique with eigensystem realization and least‑squares stiffness estimation to identify damage across varied models and excitations. The method accurately locates and quantifies damage and remains robust to simulated sensor noise, demonstrating its effectiveness in the benchmark.
A benchmark study in structural health monitoring based on simulated structural response data was developed by the joint IASC–ASCE Task Group on Structural Health Monitoring. This benchmark study was created to facilitate a comparison of various methods employed for the health monitoring of structures. The focus of the problem is simulated acceleration response data from an analytical model of an existing physical structure. Noise in the sensors is simulated in the benchmark problem by adding a stationary, broadband signal to the responses. A structural health monitoring method for determining the location and severity of damage is developed and implemented herein. The method uses the natural excitation technique in conjunction with the eigensystem realization algorithm for identification of modal parameters, and a least squares optimization to estimate the stiffness parameters. Applying this method to both undamaged and damaged response data, a comparison of results gives indication of the location and extent of damage. This method is then applied using the structural response data generated with two different models, different excitations, and various damage patterns. The proposed method is shown to be effective for damage identification. Additionally the method is found to be relatively insensitive to the simulated sensor noise.
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