@inproceedings{ce33117b0c834a7e8408102022b50359,
title = "Attitude quaternion control in the final approach phase of rendezvous and docking by sliding mode control",
abstract = "For the relative attitude control problem in phasing period of rendezvous and docking, attitude quaternion was adopted to describe the dynamic model and the kinematics equation of spacecraft. Then attitude quaternion PD feedback was designed to control the relative attitude successfully. On this basis, the sliding mode control was researched and used in relative attitude control to improve accuracy and build up anti-jamming ability. The simulation results demonstrate that sliding mode controller is more superior in rapidity and robustness.",
keywords = "attitude control, attitude quaternion, rendezvous and docking, sliding mode control",
author = "Xiaoxiao Zong and Zhenghua Liu and Yan Ren and Nan Li",
year = "2012",
doi = "10.1109/WCICA.2012.6358236",
language = "英语",
isbn = "9781467313988",
series = "Proceedings of the World Congress on Intelligent Control and Automation (WCICA)",
pages = "2177--2181",
booktitle = "WCICA 2012 - Proceedings of the 10th World Congress on Intelligent Control and Automation",
note = "10th World Congress on Intelligent Control and Automation, WCICA 2012 ; Conference date: 06-07-2012 Through 08-07-2012",
}