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...
Збережено в:
| Дата: | 2015 |
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| Автори та афіліації: |
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| Ключові слова: | keywords |
| Автори: | , |
| Формат: | Стаття |
| Мова: | Українська |
| Опубліковано: |
Інститут математики НАН України
2015
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| Онлайн доступ: | 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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Репозитарії
Transactions of Institute of Mathematics of NAS of Ukraine| Резюме: | 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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