Dynamic Modeling and Analysis of Spacecraft with Multiple Large Flexible Structures

Dynamic Modeling and Analysis of Spacecraft with Multiple Large Flexible Structures

An analytical dynamic model is presented for a spacecraft with multiple large flexible structures. Based on the partial differential equations (PDEs) of the motion of the solar panel and deployable arm, the governing equations of the main-body and deployable antenna and the boundary conditions at ea...

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Bibliographic Details
Main Authors: Jin Wei, Wei Liu, Jia Liu, Tao Yu
Format: Article
Language:English
Published: MDPI AG 2023-07-01
Series:Actuators
Subjects:
flexible structures
flexible spacecraft
global mode shapes
orthogonality relations
analytical dynamic model
dynamical characteristic
Online Access:https://www.mdpi.com/2076-0825/12/7/286

Internet

https://www.mdpi.com/2076-0825/12/7/286

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