摘要
A reachable zone generation method based on the dynamic neighborhood search is developed for landing on irregularly shaped asteroids. Firstly, the reachable zone is formulated, and a centroid distance mapping function is designed to constrain the terminal position of a trajectory with an unfixed landing point. On this basis, the reachable zone generation problem is decomposed into three sub-problems: the reference point calculating, the starting point calculating, and the boundary points searching. The reference and the starting points are solved by a trajectory optimization for minimum fuel and maximum distance, respectively. The boundary points are calculated using a guided dynamic neighborhood search method, and in each search cycle, the minimum fuel is optimized with a fixed landing point. Finally, the proposed method is verified using the 433 Eros model. The results indicate that the method is effective in generating a reachable zone on an irregular surface, efficient in searching the boundary points, and applicable to various initial positions and fuel consumptions.
投稿的翻译标题 | Reachable Zone Generation for Irregularly Shaped Asteroid Landing |
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源语言 | 繁体中文 |
页(从-至) | 1550-1558 |
页数 | 9 |
期刊 | Yuhang Xuebao/Journal of Astronautics |
卷 | 42 |
期 | 12 |
DOI | |
出版状态 | 已出版 - 30 12月 2021 |
关键词
- Asteroid landing
- Neighborhood search
- Reachable zone
- Trajectory optimization