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...
| 發表在: | Applied Sciences |
|---|---|
| Main Authors: | , , , |
| 格式: | Article |
| 語言: | 英语 |
| 出版: |
MDPI AG
2025-07-01
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| 主題: | |
| 在線閱讀: | https://www.mdpi.com/2076-3417/15/14/8064 |