Yueyang Liu, Qinglei Hu, Gang Feng 0001. Adaptive Reduced Attitude Control for Rigid Spacecraft With Elliptical Pointing Constraints. IEEE Trans. Aerospace and Electronic Systems, 59(4):3835-3847, August 2023. [doi]
@article{LiuHF23,
title = {Adaptive Reduced Attitude Control for Rigid Spacecraft With Elliptical Pointing Constraints},
author = {Yueyang Liu and Qinglei Hu and Gang Feng 0001},
year = {2023},
month = {August},
doi = {10.1109/TAES.2022.3232319},
url = {https://doi.org/10.1109/TAES.2022.3232319},
researchr = {https://researchr.org/publication/LiuHF23},
cites = {0},
citedby = {0},
journal = {IEEE Trans. Aerospace and Electronic Systems},
volume = {59},
number = {4},
pages = {3835-3847},
}