On solving the problems of optimization of trajectories of many-revolution orbit transfers of spacecraft

The problem of optimal control over many-revolution spacecraft orbit transfers between circular coplanar orbits of satellites is considered. The spacecraft flight is controlled by a thrust vector of a jet engine with restricted thrust (JERT). The mass expenditure is minimized at a limited time of fl...

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Veröffentlicht in:	Cosmic research 2006-05, Vol.44 (3), p.258-267
Hauptverfasser:	Ryzhov, S. Yu, Grigoriev, I. S.
Format:	Artikel
Sprache:	eng
Schlagworte:	Mathematical models Studies
Online-Zugang:	Volltext
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