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Titel
Time optimal control for the deployment of a tethered satellite allowing for a massive tether / Alois Steindl
VerfasserSteindl, Alois In der Gemeinsamen Normdatei der DNB nachschlagen
Erschienen in
Meccanica, Dordrecht, 2016,
Erschienen2016
Ausgabe
Published version
Umfang1 Online-Ressource (11 Seiten) : Diagramme
SpracheEnglisch
DokumenttypAufsatz in einer Zeitschrift
Schlagwörter (EN)Tethered satellite system / Deployment / Optimal control / Massive tether
ISSN1572-9648
URNurn:nbn:at:at-ubtuw:3-2684 Persistent Identifier (URN)
DOI10.1007/s11012-016-0541-9 
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Time optimal control for the deployment of a tethered satellite allowing for a massive tether [0.85 mb]
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The time optimal deployment of a satellite from a space ship is studied. In order to take the mass and lateral oscillations of the tether into account, a discretized model of the tether is build. Applying Pontryagins Maximum Principle a time-optimal deployment from a trivial downhanging configuration close to the space ship to another one farther away is computed. It is found, that the obtained solution displays a difficult switching pattern and during the variation of the initial length different kinds of bifurcations occur, leading to discontinuous variations of the optimal solution candidates.

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CC-BY-Lizenz (4.0)Creative Commons Namensnennung 4.0 International Lizenz