Nonlinear Dynamic Modeling of Satellite Cable Harness Structures

To refine the prediction of the satellite harness dynamic behavior, this paper proposes an approach to characterize and identify the nonlinearities of the harness to enrich its dynamic model. In that regard, the characterization process based on several simple experimental tests is first detailed. The nonlinear properties of the cable harness are then identified and implemented into the dynamic model treated with the distributed transfer function method. For model validation purposes, the vibration response of a piece of harness is measured experimentally using an electrodynamic shaker. The comparison between the frequency response functions obtained experimentally and numerically highlights the good predictability of the nonlinear dynamic model.

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Publication Details

Journal
Journal of Spacecraft and Rockets
Published
2024-12-28
DOI
https://doi.org/10.2514/1.a36133
Primary Topic
Vibration and Dynamic Analysis
Type
article
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article

Nonlinear Dynamic Modeling of Satellite Cable Harness Structures

Alexandre Mouysset, Aurélien Hot, Leonardo Sanches, Guilhem Michon et al.
Journal of Spacecraft and Rockets
Vibration and Dynamic Analysis
article

Nonlinear Dynamic Modeling of Satellite Cable Harness Structures

Alexandre Mouysset, Aurélien Hot, Leonardo Sanches, Guilhem Michon, Xavier Cadiot
article en

Abstract

To refine the prediction of the satellite harness dynamic behavior, this paper proposes an approach to characterize and identify the nonlinearities of the harness to enrich its dynamic model. In that regard, the characterization process based on several simple experimental tests is first detailed. The nonlinear properties of the cable harness are then identified and implemented into the dynamic model treated with the distributed transfer function method. For model validation purposes, the vibration response of a piece of harness is measured experimentally using an electrodynamic shaker. The comparison between the frequency response functions obtained experimentally and numerically highlights the good predictability of the nonlinear dynamic model.

Journal of Spacecraft and RocketsVol. 62(4)
Airbus (France) (FR), Centre National d'Études Spatiales (FR), Airbus (India) (IN), China National Space Administration (CN), National Center of Space Research and Technology (KZ), Institut Clément Ader (FR)
Openalex Percentile: Top 71%
Vibration and Dynamic Analysis
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Nonlinear Dynamic Modeling of Satellite Cable Harness Structures — Alexandre Mouysset, Aurélien Hot, et al. · Journal of Spacecraft and Rockets (2024) | TGRS Research Map | TGRS