AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
Article Link
Collect
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline
Full Length Article | Open Access

An improved equivalent beam model of large periodic beam-like space truss structures

Dongfang ZHUa,bXiaoxuan YANa,bJun SUNa,b( )Fucheng LIUa,bDongxing CAOc
Shanghai Aerospace Control Technology Institute, Shanghai 201109, China
Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai 201109, China
Faculty of Materials and Manufacturing, Beijing University of Technology, Beijing 100124, China
Show Author Information

Abstract

Space truss structures are essential components for space-based remote sensing loads with high spatial and temporal resolutions. To achieve high-precision vibration control, an accurate and efficient dynamics model is essential. In addition to the current equivalent beam model (EBM) based on the classical continuum theory, an improved equivalent beam model (IEBM) is proposed that considers the impact of the distinction between trusses and beams on torsional and shear deformations, as well as the impact of shear deformation on flexural rigidity. According to the displacement expressions of spatial beams, torsional, shear, and bending correction coefficients are introduced to derive expressions of strain energy and kinetic energy. The energy equivalence principle is then utilized to calculate the elasticity and inertia matrices, and dynamics equations are established using the finite element method. Subsequently, an IEBM is constructed by employing the particle swarm optimization approach to determine the correction coefficients with the truss natural frequency as the optimization target. The natural vibration characteristics of the structure are estimated for various material properties. Compared with the full-scale finite element model, the EBM reaches a maximum error of 80% for a low modulus of elasticity, while the maximum error of the IEBM is less than 2% for any given parameters, indicating its superior accuracy to the EBM.

Electronic Supplementary Material

Download File(s)
cja-36-12-297_ESM.pdf (729.4 KB)

References

【1】
【1】
 
 
Chinese Journal of Aeronautics
Pages 297-308

{{item.num}}

Comments on this article

Go to comment

< Back to all reports

Review Status: {{reviewData.commendedNum}} Commended , {{reviewData.revisionRequiredNum}} Revision Required , {{reviewData.notCommendedNum}} Not Commended Under Peer Review

Review Comment

Close
Close
Cite this article:
ZHU D, YAN X, SUN J, et al. An improved equivalent beam model of large periodic beam-like space truss structures. Chinese Journal of Aeronautics, 2023, 36(12): 297-308. https://doi.org/10.1016/j.cja.2023.06.034

769

Views

16

Crossref

14

Web of Science

16

Scopus

1

CSCD

Received: 17 November 2022
Revised: 06 March 2023
Accepted: 28 April 2023
Published: 13 July 2023
© 2023 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).