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| Auteurs principaux: | , , |
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| Format: | Preprint |
| Publié: |
2025
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| Accès en ligne: | https://arxiv.org/abs/2506.11435 |
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| _version_ | 1866911003556446208 |
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| author | Mao, Xuejian Liu, Pei Chen, Pei |
| author_facet | Mao, Xuejian Liu, Pei Chen, Pei |
| contents | Building and maintaining a space object catalog is necessary for space situational awareness. To realize this, one great challenge is uncooperative spacecraft maneuver detection because unknown maneuver events can lead to deviated orbital predictions and losses of tracking. Nowadays, more and more spacecraft equip electric propulsion and perform long-duration maneuvers to realize orbital transfer. Previous studies have investigated impulsive maneuver detection with space surveillance data. But, the developed method does not suffice for cases where maneuver durations are long. In this study, an improved uncooperative spacecraft maneuver detection method with space-based optical observations is proposed. Instead of a sudden maneuver event, the maneuver duration is considered. The maneuver starting/ending times are estimated along with the thrust acceleration vector. The angular residuals of nonlinear least square estimates are used to judge whether a maneuver policy could be a potential solution. The global optimum maneuver policy is chosen from multiple local minima according to the minimum-fuel principle. It is demonstrated that the maneuver duration is poorly observable if the thrust is along the orbital normal direction attributed to the nature of orbital dynamics. Real maneuver data of the Senitnel-3A spacecraft and the Senitnel-6A spacecraft is used to test the capability of the developed method. |
| format | Preprint |
| id |
arxiv_https___arxiv_org_abs_2506_11435 |
| institution | arXiv |
| publishDate | 2025 |
| record_format | arxiv |
| spellingShingle | Improved Uncooperative Spacecraft Maneuver Detection with Space-based Optical Observations Mao, Xuejian Liu, Pei Chen, Pei Optimization and Control Building and maintaining a space object catalog is necessary for space situational awareness. To realize this, one great challenge is uncooperative spacecraft maneuver detection because unknown maneuver events can lead to deviated orbital predictions and losses of tracking. Nowadays, more and more spacecraft equip electric propulsion and perform long-duration maneuvers to realize orbital transfer. Previous studies have investigated impulsive maneuver detection with space surveillance data. But, the developed method does not suffice for cases where maneuver durations are long. In this study, an improved uncooperative spacecraft maneuver detection method with space-based optical observations is proposed. Instead of a sudden maneuver event, the maneuver duration is considered. The maneuver starting/ending times are estimated along with the thrust acceleration vector. The angular residuals of nonlinear least square estimates are used to judge whether a maneuver policy could be a potential solution. The global optimum maneuver policy is chosen from multiple local minima according to the minimum-fuel principle. It is demonstrated that the maneuver duration is poorly observable if the thrust is along the orbital normal direction attributed to the nature of orbital dynamics. Real maneuver data of the Senitnel-3A spacecraft and the Senitnel-6A spacecraft is used to test the capability of the developed method. |
| title | Improved Uncooperative Spacecraft Maneuver Detection with Space-based Optical Observations |
| topic | Optimization and Control |
| url | https://arxiv.org/abs/2506.11435 |