Qinglei Hu, Boyan Jiang. Continuous Finite-Time Attitude Control for Rigid Spacecraft Based on Angular Velocity Observer. IEEE Trans. Aerospace and Electronic Systems, 54(3):1082-1092, 2018. [doi]
@article{HuJ18-0,
title = {Continuous Finite-Time Attitude Control for Rigid Spacecraft Based on Angular Velocity Observer},
author = {Qinglei Hu and Boyan Jiang},
year = {2018},
doi = {10.1109/TAES.2017.2773340},
url = {https://doi.org/10.1109/TAES.2017.2773340},
researchr = {https://researchr.org/publication/HuJ18-0},
cites = {0},
citedby = {0},
journal = {IEEE Trans. Aerospace and Electronic Systems},
volume = {54},
number = {3},
pages = {1082-1092},
}