Initial trajectory design of low-thrust spacecraft considering attitude constraints
- DOI
- 10.1038/s41598-024-70830-8
- Published
- 2024-08-30
- Container
- Scientific Reports
- Publisher
- Springer Science and Business Media LLC
- Open access
- unknown
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Cite this work
BibTeX
@article{allodium:10.1038/s41598-024-70830-8,
title = {Initial trajectory design of low-thrust spacecraft considering attitude constraints},
author = {Zichen Fan and Weiqin Ke and Ji Qi and Mingying Huo and Naiming Qi and Fei Cheng and Wenlong Li and Shaobiao Xie},
year = {2024},
journal = {Scientific Reports},
doi = {10.1038/s41598-024-70830-8},
url = {https://doi.org/10.1038/s41598-024-70830-8}
}RIS
TY - JOUR TI - Initial trajectory design of low-thrust spacecraft considering attitude constraints AU - Zichen Fan AU - Weiqin Ke AU - Ji Qi AU - Mingying Huo AU - Naiming Qi AU - Fei Cheng AU - Wenlong Li AU - Shaobiao Xie PY - 2024 JO - Scientific Reports DO - 10.1038/s41598-024-70830-8 UR - https://doi.org/10.1038/s41598-024-70830-8 ER -
APA
Fan, Z., Ke, W., Qi, J., Huo, M., Qi, N., Cheng, F., Li, W., & Xie, S. (2024). Initial trajectory design of low-thrust spacecraft considering attitude constraints. Scientific Reports. https://doi.org/10.1038/s41598-024-70830-8
Source records
- crossref · retrieved 2026-09-25T08:44:16.539Z