Abstract
Marked by the successful return of the re-entry capsule carrying 1 935. 3 grams of lunar far-side samples to Earth,the Chang’e-6 mission—the first human-executed lunar far-side sampling and return endeavor—has successfully completed all flight phases as predetermined. Serving as a backup to the prior Chang’e-5 mission on the lunar near side, and with major technical baselines unchanged,the far-side sampling and return mission introduces heightened complexity in inter-system flight planning and tracking,telemetry,and command(TT&C)coordination. For example,the lunar orbit is altered from prograde to retrograde, leading to prolonged flight durations and additional constraints; far-side communication relies on a relay satellite deployed in advance;and limited TT&C resources must be strategically allocated across diverse missions and systems. Focusing on collaborative mission design among multiple systems,the work on joint trajectory planning and TT&C relay analysis is systematically reviewed and summarized,offering valuable technical and methodological insights for future deep space exploration missions.
| Original language | English |
|---|---|
| Pages (from-to) | 1333-1344 |
| Number of pages | 12 |
| Journal | Yuhang Xuebao/Journal of Astronautics |
| Volume | 46 |
| Issue number | 7 |
| DOIs | |
| Publication status | Published - 2025 |
| Externally published | Yes |
Keywords
- Ballistic/orbital trajectory splicing
- Collaborative design
- Lunar far-side sampling and return
- Retrograde orbit
- TT&C relay communication
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