Attitude Tracking Control of Rigid Spacecraft Based on Fully Actuated System Models

التفاصيل البيبلوغرافية
العنوان: Attitude Tracking Control of Rigid Spacecraft Based on Fully Actuated System Models
المؤلفون: Liu, Quan-Zhi, Fan, Guo-Wei, Zhang, Liu, Lv, Xue-Ying, Gao, Yu, Xiao, Yang, Song, Ying
المصدر: 2023 2nd Conference on Fully Actuated System Theory and Applications (CFASTA) Fully Actuated System Theory and Applications (CFASTA), 2023 2nd Conference on. :998-1003 Jul, 2023
Relation: 2023 2nd Conference on Fully Actuated System Theory and Applications (CFASTA)
قاعدة البيانات: IEEE Xplore Digital Library
الوصف
ردمك:9798350332162
DOI:10.1109/CFASTA57821.2023.10243229