Dynamics of variable-length tethers with application to tethered satellite deployment

DOI10.1016/j.cnsns.2010.11.026zbMath1335.70026OpenAlexW2041014034MaRDI QIDQ551139

Yong-Cai Geng, Sumit K. Garg

Publication date: 13 July 2011

Published in: Communications in Nonlinear Science and Numerical Simulation (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.cnsns.2010.11.026

zbMATH Keywords

flexible multibody dynamicsabsolute nodal coordinate formulationelevator modelsatellite deploymentvariable-length tethers

Mathematics Subject Classification ID

Orbital mechanics (70M20) Dynamics of multibody systems (70E55) Strings (74K05)

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Cites Work

• Deployment/retrieval optimization for flexible tethered satellite systems
• Flexible multibody dynamics: Review of past and recent developments
• Analysis of large flexible body deformation in multibody systems using absolute coordinates
• Dynamics of sliding geometrically-exact beams: Large angle maneuver and parametric resonance
• Analysis of thin beams and cables using the absolute nodal co-ordinate formulation
• An internal damping model for the absolute nodal coordinate formulation
• Dynamics of a space vehicle with elastic deploying tether
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