Initial Values Determination of Thrust Parameters for Continuously Low-Thrust Maneuvering Spacecraft
Continuous low thrust is widely used in orbit transfer maneuvers. If the unknown maneuvers are not correctly compensated, the orbiting accuracy will be seriously affected. We propose a rapid method for pre-identifying thrust acceleration based on single-arc orbit determination in order to determine...
Tallennettuna:
| Päätekijät: | , , , |
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| Aineistotyyppi: | Artikkeli |
| Kieli: | englanti |
| Julkaistu: |
MDPI AG
2025-07-01
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| Sarja: | Applied Sciences |
| Aiheet: | |
| Linkit: | https://www.mdpi.com/2076-3417/15/14/8064 |
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