@inproceedings{47f83867873b46f7a73c5d6093841bce,
title = "Attitude controller designed based on pole assignment theory for combined spacecraft",
abstract = "This paper investigates the attitude control problem of on-orbit servicing spacecraft which changes moment of inertia after the rendezvous and docking task. Considering in the small-angle circumstance and manipulating attitude dynamics model with linearization method, the attitude controller based on pole assignment is obtained. Finally, a numerical example is provided to illustrate the effectiveness of the proposed approach.",
keywords = "Pole assignment, attitude controller, combined spacecraft, on-orbit servicing",
author = "Yan Qin and Feng Wang and Xibin Cao",
note = "Publisher Copyright: {\textcopyright} 2014 IEEE.; International Conference on Mechatronics and Control, ICMC 2014 ; Conference date: 03-07-2014 Through 05-07-2014",
year = "2015",
month = aug,
day = "31",
doi = "10.1109/ICMC.2014.7231794",
language = "英语",
series = "Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1447--1451",
booktitle = "Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014",
address = "美国",
}