Optimal control of the deployment (and retrieval) of a tethered satellite under small initial disturbances

DOI10.1007/s11012-014-9898-9zbMath1299.70053OpenAlexW2009451567MaRDI QIDQ475505

Alois Steindl

Publication date: 27 November 2014

Published in: Meccanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11012-014-9898-9

zbMATH Keywords

optimal controltethered satellite systemcenter manifoldHamiltonian Hopf bifurcation

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (3)

An analytical control law of length rate for tethered satellite system ⋮ Nonlinear Control of Tether Retrieval in an Elliptical Orbit ⋮ Chaos in a tethered satellite system induced by atmospheric drag and Earth's oblateness

Uses Software

• Mathematica

Cites Work

• Optimal control of a tethered subsatellite of three degrees of freedom
• The Hamiltonian Hopf bifurcation
• On the spectra of a family of positive matrices
• Optimal control of deployment of a tethered subsatellite
• Various Methods of Controlling the Deployment of a Tethered Satellite

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