International Space Station operational modal analysis via iterative pole relocation

Fuente: arXiv
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Main Authors: Civera, Marco, Dessena, Gabriele, Alcázar, Marina Cózar, Echániz, Saray Undiano, Bonilla-Manrique, Oscar E.
Format: Preprint
Published: 2026
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_version_ 1866913162426580992
author Civera, Marco
Dessena, Gabriele
Alcázar, Marina Cózar
Echániz, Saray Undiano
Bonilla-Manrique, Oscar E.
author_facet Civera, Marco
Dessena, Gabriele
Alcázar, Marina Cózar
Echániz, Saray Undiano
Bonilla-Manrique, Oscar E.
contents In recent years, increasing aerospace safety requirements have intensified the demand for reliable structural damage detection. This work presents an Operational Modal Analysis approach for accurate modal parameter estimation, with an application to space structure monitoring. The proposed System Identification (SI) method innovatively combines the Natural Excitation Technique (NExT) with the Fast and Relaxed Vector Fitting (FRVF) algorithm, which uses an iterative least-squares optimisation. A preliminary validation is first carried out on a numerical beam model, comparing results with analytical solutions and the established Natural Excitation Technique with Eigensystem Realisation Algorithm (NExT-ERA) and Stochastic Subspace Identification with Canonical Variate Analysis (SSI) methods. Then, operational validation is performed on real acceleration data from the Space Acceleration Measurement Systems aboard the International Space Station. Identified vibration modes from NExT-FRVF and NExT-ERA show comparable results after signal processing, with mode consistency assessed by repeated occurrence and physical interpretation, while SSI fails to identify most. The output-only algorithm proves to be highly reliable, outperforming benchmark methods under noisy conditions on a numerical system and offering reliable identifications on the experimental data.
format Preprint
id arxiv_https___arxiv_org_abs_2605_26257
institution arXiv
publishDate 2026
record_format arxiv
spellingShingle International Space Station operational modal analysis via iterative pole relocation
Civera, Marco
Dessena, Gabriele
Alcázar, Marina Cózar
Echániz, Saray Undiano
Bonilla-Manrique, Oscar E.
Signal Processing
Systems and Control
In recent years, increasing aerospace safety requirements have intensified the demand for reliable structural damage detection. This work presents an Operational Modal Analysis approach for accurate modal parameter estimation, with an application to space structure monitoring. The proposed System Identification (SI) method innovatively combines the Natural Excitation Technique (NExT) with the Fast and Relaxed Vector Fitting (FRVF) algorithm, which uses an iterative least-squares optimisation. A preliminary validation is first carried out on a numerical beam model, comparing results with analytical solutions and the established Natural Excitation Technique with Eigensystem Realisation Algorithm (NExT-ERA) and Stochastic Subspace Identification with Canonical Variate Analysis (SSI) methods. Then, operational validation is performed on real acceleration data from the Space Acceleration Measurement Systems aboard the International Space Station. Identified vibration modes from NExT-FRVF and NExT-ERA show comparable results after signal processing, with mode consistency assessed by repeated occurrence and physical interpretation, while SSI fails to identify most. The output-only algorithm proves to be highly reliable, outperforming benchmark methods under noisy conditions on a numerical system and offering reliable identifications on the experimental data.
title International Space Station operational modal analysis via iterative pole relocation
topic Signal Processing
Systems and Control
url https://arxiv.org/abs/2605.26257