Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method
The task of optimizing the space vehicle combined orbital plane change maneuver with the aim of maximizing its final mass is considered in the paper. Burst of power is used for the vehicles exit from the initial low earth orbit and subsequent re-entry. Starting from atmospheric entry till the end of...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Samara National Research University
2018-07-01
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| Series: | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
| Subjects: | |
| Online Access: | https://journals.ssau.ru/vestnik/article/viewFile/6216/6106 |