Optimal control of deployment of a tethered subsatellite

DOI10.1023/A:1022956002484zbMath1036.70015OpenAlexW1570523361MaRDI QIDQ1415685

Alois Steindl, Hans Troger

Publication date: 9 December 2003

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

Full work available at URL: https://doi.org/10.1023/a:1022956002484

zbMATH Keywords

Pontryagin's maximum principlestate constrainttime optimal solution

Mathematics Subject Classification ID

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

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Optimal control of a tethered subsatellite of three degrees of freedom ⋮ Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations ⋮ Nonlinear Control of Tether Retrieval in an Elliptical Orbit ⋮ Advances in dynamics and control of tethered satellite systems ⋮ Modelling, dynamics and control of tethered satellite systems ⋮ Three-dimensional optimal deployment of a tethered subsatellite with an elastic tether ⋮ Optimal control of the deployment (and retrieval) of a tethered satellite under small initial disturbances ⋮ Multi-scale continuum mechanics: From global bifurcations to noise induced high-dimensional chaos ⋮ An \(hp\) symplectic pseudospectral method for nonlinear optimal control ⋮ Analysis of the dynamics of the formation of a tether group of three nanosatellites taking into account their motion around the centers of mass ⋮ Tethered satellite systems: A challenge for mechanics and applied mathematics ⋮ A novel underactuated control scheme for deployment/retrieval of space tethered system

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