Optimizing flight trajectories for space vehicles with an additional fuel tank. I

We consider optimization problems for spatial trajectories of space flights for space vehicles with an additional fuel tank from a low circular orbit of a man-made Earth satellite to a geotransitional orbit. The motion of the space vehicle is controlled through a jet engine with bounded thrust. To d...

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Veröffentlicht in:Automation and remote control 2017-12, Vol.78 (12), p.2203-2210
Hauptverfasser: Grigoriev, I. S., Danilina, I. A.
Format: Artikel
Sprache:eng
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