Robust Saturated Finite-Time Attitude Control for Spacecraft Using Integral Sliding Mode

被引：53
|
作者：
Guo, Yong [1 ,3 ]
Huang, Bing [1 ,3 ]
Song, Shen-min [2 ]
Li, Ai-jun [1 ,3 ]
Wang, Chang-qing [1 ,3 ]
机构：
[1] Northwestern Polytech Univ, Xian 710129, Shaanxi, Peoples R China
[2] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150001, Heilongjiang, Peoples R China
[3] Sch Automat, 127 Youyi West Rd, Beilin, Shaanxi, Peoples R China
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2019年 / 42卷 / 02期
基金：
中国国家自然科学基金;
关键词：
OUTPUT-FEEDBACK; RIGID SPACECRAFT; TRACKING CONTROL; COORDINATION CONTROL; STABILIZATION;
D O I：
10.2514/1.G003520
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：440 / 446
页数：7
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