Dual-Quaternion-Based Spacecraft Autonomous Rendezvous and Docking Under Six-Degree-of-Freedom Motion Constraints
出版年份 2018 全文链接
标题
Dual-Quaternion-Based Spacecraft Autonomous Rendezvous and Docking Under Six-Degree-of-Freedom Motion Constraints
作者
关键词
-
出版物
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
Volume 41, Issue 5, Pages 1150-1162
出版商
American Institute of Aeronautics and Astronautics (AIAA)
发表日期
2017-12-15
DOI
10.2514/1.g003094
参考文献
相关参考文献
注意:仅列出部分参考文献,下载原文获取全部文献信息。- Observer-Based Fault-Tolerant Attitude Control for Rigid Spacecraft
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