@inproceedings{d428db22fdf845a3b8eba10ff6817172,
title = "Quaternion-based fuzzy attitude regulation of a rigid spacecraft",
abstract = "The main problem addressed was the quaternion-based, attitude regulation of a rigid spacecraft in the presence of external disturbances. A model-based fuzzy attitude control scheme was presented. The parallel distributed compensation was employed to arrive at a controller that guaranteed the stability of closed-loop system and performance specifications in terms of constraints on input and disturbance rejection. Both the stability and control performance were incorporated in the linear matrix inequality (LMI) conditions. The feedback gains were obtained by the convex optimization technique based on LMI. Simulation results demonstrate that the proposed control scheme is efficient.",
keywords = "Convex optimization, Fuzzy control, Linear matrix inequality, Quaternion feedback, Spacecraft attitude regulation",
author = "Bin Song and Guangfu Ma and Chuanjiang Li and Jianting Lv",
year = "2006",
doi = "10.1109/WCICA.2006.1713623",
language = "英语",
isbn = "1424403324",
series = "Proceedings of the World Congress on Intelligent Control and Automation (WCICA)",
pages = "8434--8438",
booktitle = "Proceedings of the World Congress on Intelligent Control and Automation (WCICA)",
note = "6th World Congress on Intelligent Control and Automation, WCICA 2006 ; Conference date: 21-06-2006 Through 23-06-2006",
}