De-spinning of tethered space target via partially invariable deployment with tension control

DOI10.1007/S11071-019-04811-2zbMath1437.93095OpenAlexW2913628179WikidataQ128436554 ScholiaQ128436554MaRDI QIDQ783509

Dongping Jin, Hao Wen

Publication date: 4 August 2020

Published in: Nonlinear Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11071-019-04811-2

zbMATH Keywords

tension controldeploymentde-spinpartially invariablespace tether

Mathematics Subject Classification ID

Automated systems (robots, etc.) in control theory (93C85)

Related Items (1)

Dynamics of a flexible multi-tethered satellite formation in a halo orbit with uncertain parameters

Uses Software

• Ipopt

Cites Work

• Advances in dynamics and control of tethered satellite systems
• On the implementation of an interior-point filter line-search algorithm for large-scale nonlinear programming
• Postcapture robust nonlinear control for tethered space robot with constraints on actuator and velocity of space tether

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