Rigid–Flexible–Thermal Coupling Dynamics for Spacecraft with a Composite-Laminated Solar Array in a Space Thermal Environment

dc.contributor.author	Zhang, Wei
dc.contributor.author	Zhang, Shijie
dc.contributor.author	Dong, Zezheng
dc.contributor.author	Wang, Haibo
dc.contributor.author	Yang, Dalin
dc.contributor.author	Chen, Ming
dc.contributor.author	Liu, Xiangzhen
dc.date.accessioned	2026-08-20T21:13:50Z
dc.date.available	2026-08-20T21:13:50Z
dc.date.copyright	2025/11/18
dc.date.issued	2026
dc.identifier.other	JAEEEZ.ASENG-6304.pdf
dc.identifier.uri	http://yetl.yabesh.ir/yetl1/handle/yetl/4314152
dc.description.abstract	AbstractThis paper proposes a rigid–flexible–thermal coupling dynamics model for a spacecraft with a composite-laminated solar array in a space thermal environment, and the thermally induced vibration on the spacecraft is studied. The spacecraft system ...
dc.publisher	American Society of Civil Engineers
dc.title	Rigid–Flexible–Thermal Coupling Dynamics for Spacecraft with a Composite-Laminated Solar Array in a Space Thermal Environment
dc.type	Journal Article
dc.journal.volume	39
dc.journal.issue	2
dc.journal.title	Journal of Aerospace Engineering
dc.identifier.doi	10.1061/JAEEEZ.ASENG-6304
dc.journal.fristpage	04025123-1
dc.journal.lastpage	04025123-22
dc.page	22
dc.tree	Journal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 002
dc.contenttype	Fulltext