Mode Weighting Method for modeling and internal resonance of spatial folded beams

Spatial folded beams, exemplified by the locked configuration of spatial manipulators, enable more complex spatial operations than planar structures but exhibit strong couplings and high-dimensional characteristics that complicate modeling and control. In this study, the Mode Weighting Method (MWM) is developed for spatial assembled structures, enabling efficient extraction of spatially coupled modes and the construction of low-dimensional nonlinear dynamic models. The MWM defines flexible component orientations using Euler angles and models joints as artificial springs. It constructs the assumed mode (AM) model from individual component modes, then extracts spatially coupled global modes via mode weighting to establish a global mode (GM) model with joint nonlinearity. This reduced GM model accurately captures the complex structural coupling, as validated through finite element (FE) analysis and physical experiments. Compared with the FEM, the MWM achieves comparable accuracy with 75% fewer degrees of freedom and a 99.36% reduction in computation time for the computation of the first ten natural frequencies of the standard spatial four-folded beam under the same computational settings. Variations in Euler angles lead spatial structures to display richer internal resonances, including those between adjacent and separated frequencies, as well as more mode transitions. In some cases, internal resonance amplifies local vibrations to 1.8 times the linear level, threatening structural safety. By leveraging Euler angles, the GM model is well-suited for attitude-adjustable aerospace structures, while the MWM provides a concise analytical framework readily extendable to arbitrary spatial assembled structures. • A Mode Weighting Method (MWM) is developed for low-dimensional nonlinear modeling of spatial assembled structures. • The proposed MWM is validated by both finite element analysis and experiments. • For a spatial four-folded beam, the MWM achieves FEM-level accuracy with 75% fewer DoFs. • Internal resonance induces multi-frequency responses and amplifies local vibration up to 1.8 times.

Authors

Institutions

Publication Details

Journal
Engineering Structures
Published
2026-03-14
DOI
https://doi.org/10.1016/j.engstruct.2026.122511
Primary Topic
Aeroelasticity and Vibration Control
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Mode Weighting Method for modeling and internal resonance of spatial folded beams

Yan Xu, Yilong Wang, Marco Amabili, Xiaoyun Zhang et al.
Engineering Structures
Aeroelasticity and Vibration Control
article

Mode Weighting Method for modeling and internal resonance of spatial folded beams

Yan Xu, Yilong Wang, Marco Amabili, Xiaoyun Zhang, Chao Chen, Dengqing Cao
article en

Abstract

Spatial folded beams, exemplified by the locked configuration of spatial manipulators, enable more complex spatial operations than planar structures but exhibit strong couplings and high-dimensional characteristics that complicate modeling and control. In this study, the Mode Weighting Method (MWM) is developed for spatial assembled structures, enabling efficient extraction of spatially coupled modes and the construction of low-dimensional nonlinear dynamic models. The MWM defines flexible component orientations using Euler angles and models joints as artificial springs. It constructs the assumed mode (AM) model from individual component modes, then extracts spatially coupled global modes via mode weighting to establish a global mode (GM) model with joint nonlinearity. This reduced GM model accurately captures the complex structural coupling, as validated through finite element (FE) analysis and physical experiments. Compared with the FEM, the MWM achieves comparable accuracy with 75% fewer degrees of freedom and a 99.36% reduction in computation time for the computation of the first ten natural frequencies of the standard spatial four-folded beam under the same computational settings. Variations in Euler angles lead spatial structures to display richer internal resonances, including those between adjacent and separated frequencies, as well as more mode transitions. In some cases, internal resonance amplifies local vibrations to 1.8 times the linear level, threatening structural safety. By leveraging Euler angles, the GM model is well-suited for attitude-adjustable aerospace structures, while the MWM provides a concise analytical framework readily extendable to arbitrary spatial assembled structures. • A Mode Weighting Method (MWM) is developed for low-dimensional nonlinear modeling of spatial assembled structures. • The proposed MWM is validated by both finite element analysis and experiments. • For a spatial four-folded beam, the MWM achieves FEM-level accuracy with 75% fewer DoFs. • Internal resonance induces multi-frequency responses and amplifies local vibration up to 1.8 times.

Engineering StructuresVol. 357
Shandong University of Technology (CN), Northwestern Polytechnical University (CN), Harbin Institute of Technology (CN), Westlake University (CN), McGill University (CA)
Peace, Justice and strong institutions
Openalex Percentile: Top 21%
Aeroelasticity and Vibration Control
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.