An analytical control law of length rate for tethered satellite system

DOI10.1007/S11012-016-0567-ZzbMath1375.70080OpenAlexW2540450191MaRDI QIDQ2399265

Yanyan Li

Publication date: 22 August 2017

Published in: Meccanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11012-016-0567-z

zbMATH Keywords

stabilitytethered satellite systemdeploymentanalytical control lawlength rate control

Mathematics Subject Classification ID

Application models in control theory (93C95) Asymptotic stability in control theory (93D20) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Cites Work

• Nonlinear dynamic analysis of a three-body tethered satellite system with deployment/retrieval
• Optimal control of the deployment (and retrieval) of a tethered satellite under small initial disturbances
• Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations
• Deployment/retrieval optimization for flexible tethered satellite systems
• Cell-to-cell mapping. A method of global analysis for nonlinear systems
• Adaptive neural control of the deployment procedure for tether-assisted re-entry
• Various Methods of Controlling the Deployment of a Tethered Satellite

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