@inproceedings{4c82dd07f33f409c80cd4ea978a0e26f,
title = "Robust finite-time control of coupled spacecraft using dual quaternion",
abstract = "A novel terminal sliding control scheme is proposed to solve the coordinated control problem of coupled spacecraft. The integrated translational and rotational dynamics is employed using dual quaternion. A model-independent terminal sliding controller is further proposed such that the defined dynamical synchronization error can converge to the desired trajectory in finite time. Numerical simulations demonstrate the effectiveness of the proposed method.",
keywords = "coupled spacecraft dynamics, dual quaternion, finite time, integrated translation and rotation, sliding control",
author = "Zhao Wen and Dong Yunfeng",
note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 3rd IEEE International Conference on Control Science and Systems Engineering, ICCSSE 2017 ; Conference date: 17-08-2017 Through 19-08-2017",
year = "2017",
month = oct,
day = "26",
doi = "10.1109/CCSSE.2017.8087900",
language = "英语",
series = "2017 3rd IEEE International Conference on Control Science and Systems Engineering, ICCSSE 2017",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "87--91",
booktitle = "2017 3rd IEEE International Conference on Control Science and Systems Engineering, ICCSSE 2017",
address = "美国",
}