摘要
Focusing on the high landing safety and accuracy requirements in future planetary landing and sample return missions, the landing dynamic environment and constraints of planetary atmospheric entry and powered descent landing are analyzed. Then, research progress of the planetary landing trajectory optimizations is reviewed. Based on the characteristics of planetary landing trajectory optimization, the key techniques are summarized on the transformation of nonlinear dynamics, optimal trajectory rapid solving under complex constraints, and reachability/controllability analysis under uncertainty.
投稿的翻译标题 | Research Progress of Planetary Landing Trajectory Optimization Techniques |
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源语言 | 繁体中文 |
页(从-至) | 677-686 |
页数 | 10 |
期刊 | Yuhang Xuebao/Journal of Astronautics |
卷 | 42 |
期 | 6 |
DOI | |
出版状态 | 已出版 - 30 6月 2021 |
关键词
- Asteroid soft landing
- Atmospheric entry
- Planetary landing
- Powered descent
- Trajectory optimization