Zeming Hao, Haifeng Hu 0012, Yong He, Huifeng Li. Reachable-Orbit-Domain for Launch Vehicles Based on Polyhedron Approximation Method. In 13th Asian Control Conference, ASCC 2022, Jeju, Korea, May 4-7, 2022. pages 2447-2449, IEEE, 2022. [doi]
@inproceedings{HaoHHL22,
title = {Reachable-Orbit-Domain for Launch Vehicles Based on Polyhedron Approximation Method},
author = {Zeming Hao and Haifeng Hu 0012 and Yong He and Huifeng Li},
year = {2022},
doi = {10.23919/ASCC56756.2022.9828333},
url = {https://doi.org/10.23919/ASCC56756.2022.9828333},
researchr = {https://researchr.org/publication/HaoHHL22},
cites = {0},
citedby = {0},
pages = {2447-2449},
booktitle = {13th Asian Control Conference, ASCC 2022, Jeju, Korea, May 4-7, 2022},
publisher = {IEEE},
isbn = {978-89-93215-23-6},
}