Rigid-flexible coupled dynamics and configuration stability of maneuverable space tether net under impact loads

This paper investigates the configuration stability and rigid–flexible coupled dynamics of maneuverable space tether nets under impact loads. To analyze the complex 3D maneuvers of the net, a geometric mechanics framework is developed, incorporating the rigid–flexible coupling between wave propagation in the net and the attitude dynamics of maneuvering satellites attached to its corners. A coordinate-free representation in Lie group is derived for the satellites’ attitude dynamics on SO ( 3 ) . Equilibrium states, modal shapes, and chaotic behavior of the tether net are examined using the geometric Jacobian method, which reveals the coexistence of stiff tether dynamics and slow satellite attitude motions, leading to extreme disparities in time scales and makes numerical analysis challenging by conventional integration schemes. To solve the problem, a structure-preserving integrator is derived to accurately analyze the chaotic behavior of the net over extended periods. Dynamic responses to impact loads are analyzed under two initial conditions: (i) a slack net and (ii) a net tensioned by satellite control forces and torques. Numerical results reveal significant coupling effects between net deformation and satellite attitude motion, and even minor perturbations may lead to chaotic responses of the net indicated by Lyapunov exponents. Moreover, the pre-tension of the net by control forces from satellites can effectively suppress chaotic behaviors, leading to more stable configuration and controlled maneuvering. These findings offer critical insights into configuration stability and dynamics of maneuverable space tether nets, which will enable the effective control strategy development to suppress chaos and enhance net’s maneuverability in three-dimensional space. • Investigated equilibrium, modal shapes, and chaos in maneuverable space tether nets. • Modeled attitude dynamics by Lie-group theory for 3D maneuvering. • Developed a variational integrator for accurate long-term chaotic behavior simulation. • Applied geometric Jacobian for linearized modal analysis of equilibrium states.

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Publication Details

Journal
Acta Astronautica
Published
2025-03-07
DOI
https://doi.org/10.1016/j.actaastro.2025.02.031
Citations
4
Primary Topic
Space Satellite Systems and Control
Type
article
Field-Weighted Citation Impact
19.97

Funders

Controls
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article

Rigid-flexible coupled dynamics and configuration stability of maneuverable space tether net under impact loads

Mani Kakavand, Zheng Hong Zhu
4 citations
Acta Astronautica
Space Satellite Systems and Control
19.97
article

Rigid-flexible coupled dynamics and configuration stability of maneuverable space tether net under impact loads

Mani Kakavand, Zheng Hong Zhu
article en
4 citations

Abstract

This paper investigates the configuration stability and rigid–flexible coupled dynamics of maneuverable space tether nets under impact loads. To analyze the complex 3D maneuvers of the net, a geometric mechanics framework is developed, incorporating the rigid–flexible coupling between wave propagation in the net and the attitude dynamics of maneuvering satellites attached to its corners. A coordinate-free representation in Lie group is derived for the satellites’ attitude dynamics on SO ( 3 ) . Equilibrium states, modal shapes, and chaotic behavior of the tether net are examined using the geometric Jacobian method, which reveals the coexistence of stiff tether dynamics and slow satellite attitude motions, leading to extreme disparities in time scales and makes numerical analysis challenging by conventional integration schemes. To solve the problem, a structure-preserving integrator is derived to accurately analyze the chaotic behavior of the net over extended periods. Dynamic responses to impact loads are analyzed under two initial conditions: (i) a slack net and (ii) a net tensioned by satellite control forces and torques. Numerical results reveal significant coupling effects between net deformation and satellite attitude motion, and even minor perturbations may lead to chaotic responses of the net indicated by Lyapunov exponents. Moreover, the pre-tension of the net by control forces from satellites can effectively suppress chaotic behaviors, leading to more stable configuration and controlled maneuvering. These findings offer critical insights into configuration stability and dynamics of maneuverable space tether nets, which will enable the effective control strategy development to suppress chaos and enhance net’s maneuverability in three-dimensional space. • Investigated equilibrium, modal shapes, and chaos in maneuverable space tether nets. • Modeled attitude dynamics by Lie-group theory for 3D maneuvering. • Developed a variational integrator for accurate long-term chaotic behavior simulation. • Applied geometric Jacobian for linearized modal analysis of equilibrium states.

Acta AstronauticaVol. 232
York University (CA)
Natural Sciences and Engineering Research Council of Canada
Affordable and clean energy
Openalex Percentile: Top 1%
Space Satellite Systems and Control
19.97
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