Comment on "Robust Saturated Finite Time Output Feedback Attitude Stabilization for Rigid Spacecraft"

被引：1
|
作者：
Su, Yuxin [1 ]
机构：
[1] Xidian Univ, Sch Electmech Engn, Xian 710071, Peoples R China
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2017年 / 40卷 / 06期
关键词：
D O I：
10.2514/1.G001555
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：1537 / 1537
页数：1
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