TY - JOUR
T1 - Thermal vibration analysis of cables in tensegrity during space deployment
AU - Zou, Haoran
AU - Boni, Luisa
AU - Fu, zeyu
AU - Quarta, Alessandro A.
AU - Han, Fei
AU - Deng, Zichen
N1 - Publisher Copyright:
© 2025 Elsevier Ltd
PY - 2025/11/10
Y1 - 2025/11/10
N2 - This paper presents a dynamic model for cables in tensegrity modules during space deployment, accounting for the combined effects of mechanical forces and thermal loads in the space environment. Key factors such as Coriolis and gyroscopic forces, dynamic stiffening, and coupling between rotation, axial motion and flexible deformation are integrated to characterize dynamic behavior and structural response of the considered cables. Frequencies and modal shapes of representative cable members are derived precisely using dynamic stiffness theory and their dynamic response under space thermal effects is analyzed through a model with accuracy experimentally substantiated. Furthermore, the impact of variable initial stresses, deployment duration, and thermal flux incidence angles on the dynamic behavior of representative members is examined in detail. The results obtained in this study reveal the evolutionary dynamics of tensegrity modules during space deployment, offering valuable insights for the assembly and construction of ultra-large spacecraft.
AB - This paper presents a dynamic model for cables in tensegrity modules during space deployment, accounting for the combined effects of mechanical forces and thermal loads in the space environment. Key factors such as Coriolis and gyroscopic forces, dynamic stiffening, and coupling between rotation, axial motion and flexible deformation are integrated to characterize dynamic behavior and structural response of the considered cables. Frequencies and modal shapes of representative cable members are derived precisely using dynamic stiffness theory and their dynamic response under space thermal effects is analyzed through a model with accuracy experimentally substantiated. Furthermore, the impact of variable initial stresses, deployment duration, and thermal flux incidence angles on the dynamic behavior of representative members is examined in detail. The results obtained in this study reveal the evolutionary dynamics of tensegrity modules during space deployment, offering valuable insights for the assembly and construction of ultra-large spacecraft.
KW - Dynamic stiffness method
KW - Space deployment
KW - Tensegrity
KW - Thermal vibration
UR - http://www.scopus.com/inward/record.url?scp=105006979409&partnerID=8YFLogxK
U2 - 10.1016/j.jsv.2025.119208
DO - 10.1016/j.jsv.2025.119208
M3 - 文章
AN - SCOPUS:105006979409
SN - 0022-460X
VL - 616
JO - Journal of Sound and Vibration
JF - Journal of Sound and Vibration
M1 - 119208
ER -