Thermal alternation induced vibration analysis of spacecraft with lateral solar arrays in orbit

DOI10.1016/J.APM.2020.05.008zbMath1481.70096OpenAlexW3028477916MaRDI QIDQ2049751

Lun Liu, Yuteng Cao, Guiqin He, Dengqing Cao

Publication date: 27 August 2021

Published in: Applied Mathematical Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.apm.2020.05.008

zbMATH Keywords

spacecraftlateral solar arraysmulti-rigid-flexible bodiesrigid-flexible-thermal couplingthermal alternation

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Cites Work

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• Thermoacoustic response of a simply supported isotropic rectangular plate in graded thermal environments
• Global mode method for dynamic modeling of a flexible-link flexible-joint manipulator with tip mass
• Vibration analysis of FG spinning beam using higher-order shear deformation beam theory in thermal environment
• Nonlinear vibration analysis of FG nano-beams resting on elastic foundation in thermal environment using stress-driven nonlocal integral model
• Thermal vibration analysis of functionally graded shallow spherical caps by introducing a decoupling analytical approach
• Dynamical modeling and attitude analysis for the spacecraft with lateral solar arrays
• Two kinds of tube elements for transient thermal–structural analysis of large space structures

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