A Deformation Reconstruction Strategy for Integrated Truss Structures Subjected to Thermal–Mechanical Load

The deformation monitoring of integrated truss structures (ITSs) is essential for ensuring the reliable performance of mounted equipment in complex space environments. Reconstruction methods based on local strain information have been proven effective, yet the identification faces significant challe...

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Main Authors: Zexing Yu, Xiaofei Ma, Jialong Zhu, Dayu Zhang, Yonggang Xue, Pengfei Huang, Yichen Li, Hao Li
Format: Article
Language:English
Published: MDPI AG 2025-01-01
Series:Sensors
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Online Access:https://www.mdpi.com/1424-8220/25/2/558
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author Zexing Yu
Xiaofei Ma
Jialong Zhu
Dayu Zhang
Yonggang Xue
Pengfei Huang
Yichen Li
Hao Li
author_facet Zexing Yu
Xiaofei Ma
Jialong Zhu
Dayu Zhang
Yonggang Xue
Pengfei Huang
Yichen Li
Hao Li
author_sort Zexing Yu
collection DOAJ
description The deformation monitoring of integrated truss structures (ITSs) is essential for ensuring the reliable performance of mounted equipment in complex space environments. Reconstruction methods based on local strain information have been proven effective, yet the identification faces significant challenges due to variable thermal–mechanical loads, interactions among structural components, and special boundary conditions. This paper proposes a deformation reconstruction strategy tailored for ITSs under combined thermal–mechanical load scenarios wherein deformations of both the primary truss structures and the attached panel systems are investigated. The proposed approach utilizes Ko displacement theory as the core algorithm, while the least squares optimization method is employed to determine the integration with unknown initial values during the reconstruction process. Validation is conducted through diverse load scenarios, and the reconstruction results are evaluated using errors based on the root mean square. The result demonstrates that the proposed method can reconstruct deformations of truss structures under both mechanical and thermal loads. Furthermore, the optimization-based approach achieves accurate reconstructed results in the case of panels with two-point fixed boundary conditions. This study provides an effective strategy for in-orbit deformation reconstruction, addressing challenges posed by complex loads and structural configurations.
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institution Kabale University
issn 1424-8220
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publishDate 2025-01-01
publisher MDPI AG
record_format Article
series Sensors
spelling doaj-art-6efd5eff139642579c8609a98193b9632025-01-24T13:49:20ZengMDPI AGSensors1424-82202025-01-0125255810.3390/s25020558A Deformation Reconstruction Strategy for Integrated Truss Structures Subjected to Thermal–Mechanical LoadZexing Yu0Xiaofei Ma1Jialong Zhu2Dayu Zhang3Yonggang Xue4Pengfei Huang5Yichen Li6Hao Li7Xi’an Institute of Space Radio Technology, Xi’an 710100, ChinaXi’an Institute of Space Radio Technology, Xi’an 710100, ChinaXi’an Institute of Space Radio Technology, Xi’an 710100, ChinaXi’an Institute of Space Radio Technology, Xi’an 710100, ChinaXi’an Institute of Space Radio Technology, Xi’an 710100, ChinaXi’an Institute of Space Radio Technology, Xi’an 710100, ChinaXi’an Institute of Space Radio Technology, Xi’an 710100, ChinaXi’an Institute of Space Radio Technology, Xi’an 710100, ChinaThe deformation monitoring of integrated truss structures (ITSs) is essential for ensuring the reliable performance of mounted equipment in complex space environments. Reconstruction methods based on local strain information have been proven effective, yet the identification faces significant challenges due to variable thermal–mechanical loads, interactions among structural components, and special boundary conditions. This paper proposes a deformation reconstruction strategy tailored for ITSs under combined thermal–mechanical load scenarios wherein deformations of both the primary truss structures and the attached panel systems are investigated. The proposed approach utilizes Ko displacement theory as the core algorithm, while the least squares optimization method is employed to determine the integration with unknown initial values during the reconstruction process. Validation is conducted through diverse load scenarios, and the reconstruction results are evaluated using errors based on the root mean square. The result demonstrates that the proposed method can reconstruct deformations of truss structures under both mechanical and thermal loads. Furthermore, the optimization-based approach achieves accurate reconstructed results in the case of panels with two-point fixed boundary conditions. This study provides an effective strategy for in-orbit deformation reconstruction, addressing challenges posed by complex loads and structural configurations.https://www.mdpi.com/1424-8220/25/2/558deformation reconstructionlarge space trussthermal–mechanical loadKo displacement theorystructural health monitoring
spellingShingle Zexing Yu
Xiaofei Ma
Jialong Zhu
Dayu Zhang
Yonggang Xue
Pengfei Huang
Yichen Li
Hao Li
A Deformation Reconstruction Strategy for Integrated Truss Structures Subjected to Thermal–Mechanical Load
Sensors
deformation reconstruction
large space truss
thermal–mechanical load
Ko displacement theory
structural health monitoring
title A Deformation Reconstruction Strategy for Integrated Truss Structures Subjected to Thermal–Mechanical Load
title_full A Deformation Reconstruction Strategy for Integrated Truss Structures Subjected to Thermal–Mechanical Load
title_fullStr A Deformation Reconstruction Strategy for Integrated Truss Structures Subjected to Thermal–Mechanical Load
title_full_unstemmed A Deformation Reconstruction Strategy for Integrated Truss Structures Subjected to Thermal–Mechanical Load
title_short A Deformation Reconstruction Strategy for Integrated Truss Structures Subjected to Thermal–Mechanical Load
title_sort deformation reconstruction strategy for integrated truss structures subjected to thermal mechanical load
topic deformation reconstruction
large space truss
thermal–mechanical load
Ko displacement theory
structural health monitoring
url https://www.mdpi.com/1424-8220/25/2/558
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