Li-Gang Gong, Qing Wang, Chaoyang Dong. Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming. J. Franklin Institute, 356(10):4971-5000, 2019. [doi]
@article{GongWD19,
title = {Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming},
author = {Li-Gang Gong and Qing Wang and Chaoyang Dong},
year = {2019},
doi = {10.1016/j.jfranklin.2019.04.018},
url = {https://doi.org/10.1016/j.jfranklin.2019.04.018},
researchr = {https://researchr.org/publication/GongWD19},
cites = {0},
citedby = {0},
journal = {J. Franklin Institute},
volume = {356},
number = {10},
pages = {4971-5000},
}