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 |
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| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | Ukrainisch |
| Veröffentlicht: |
Інститут математики НАН України
2015
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| 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 |
| Завантажити файл: |  |