A simulation of the Four-way lunar Lander–Orbiter tracking mode for the Chang’E-5 mission
- DOI
- 10.1016/j.asr.2016.03.007
- Published
- 2016-06
- Container
- Advances in Space Research
- Publisher
- Elsevier BV
- Open access
- unknown
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Cite this work
BibTeX
@article{allodium:10.1016/j.asr.2016.03.007,
title = {A simulation of the Four-way lunar Lander–Orbiter tracking mode for the Chang’E-5 mission},
author = {Fei Li and Mao Ye and Jianguo Yan and Weifeng Hao and Jean-Pierre Barriot},
year = {2016},
journal = {Advances in Space Research},
doi = {10.1016/j.asr.2016.03.007},
url = {https://doi.org/10.1016/j.asr.2016.03.007}
}RIS
TY - JOUR TI - A simulation of the Four-way lunar Lander–Orbiter tracking mode for the Chang’E-5 mission AU - Fei Li AU - Mao Ye AU - Jianguo Yan AU - Weifeng Hao AU - Jean-Pierre Barriot PY - 2016 JO - Advances in Space Research DO - 10.1016/j.asr.2016.03.007 UR - https://doi.org/10.1016/j.asr.2016.03.007 ER -
APA
Li, F., Ye, M., Yan, J., Hao, W., & Barriot, J. (2016). A simulation of the Four-way lunar Lander–Orbiter tracking mode for the Chang’E-5 mission. Advances in Space Research. https://doi.org/10.1016/j.asr.2016.03.007
Source records
- crossref · retrieved 2026-09-25T09:24:24.058Z