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A method for the constructing of optimal trajectories in a strictly central gravity field

A novel method for constructing optimal flight trajectories of an electricpropulsion spacecraft between far elliptical orbits in a central gravitationalfield is developed. An optimisation of the flight from the low Earth orbit toan almost geostationary orbit is done. For this maneuver, the payload m...

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Datum:2015
Автори та афіліації:
  • Б. М. Кіфоренко — Iнститут механiки iм. С.П. Тимошенка НАН України
  • Я. В. Ткаченко — Iнститут механiки iм. С.П. Тимошенка НАН України
Ключові слова:keywords
Hauptverfasser: Кіфоренко, Б. М., Ткаченко, Я. В.
Format: Artikel
Sprache:Ukrainisch
Veröffentlicht: Інститут математики НАН України 2015
Online Zugang:https://trim.imath.kiev.ua/index.php/trim/article/view/23
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Назва журналу:Transactions of Institute of Mathematics of NAS of Ukraine
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Transactions of Institute of Mathematics of NAS of Ukraine
Beschreibung
Zusammenfassung:A novel method for constructing optimal flight trajectories of an electricpropulsion spacecraft between far elliptical orbits in a central gravitationalfield is developed. An optimisation of the flight from the low Earth orbit toan almost geostationary orbit is done. For this maneuver, the payload massincrease affected by an energy storage in the engine system is estimated.

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