Saturated Output Feedback Control for Global Asymptotic Attitude Tracking of Spacecraft

被引：12
作者：
Xia, Yuquan [1 ]
Su, Yuxin [1 ]
机构：
[1] Xidian Univ, Sch Electromech Engn, Xian 710071, Shaanxi, Peoples R China
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2018年 / 41卷 / 10期
关键词：
ANGULAR VELOCITY-MEASUREMENT; CONTROL INPUT SATURATION; RIGID SPACECRAFT; CONTROL DESIGN; STABILIZATION; SYSTEMS; BODIES;
D O I：
10.2514/1.G003566
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
[No abstract available]
引用
收藏
页码：2298 / +
页数：8
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