Observer-Based Fault-Tolerant Attitude Control for Spacecraft with Input Delay

被引：46
|
作者：
Liu, Chuang [1 ,2 ]
Vukovich, George [2 ]
Sun, Zhaowei [1 ]
Shi, Keke [1 ]
机构：
[1] Harbin Inst Technol, Res Ctr Satellite Technol, 2 Yikuang St, Harbin 150001, Heilongjiang, Peoples R China
[2] York Univ, Dept Earth & Space Sci & Engn, 4700 Keele Str, Toronto, ON M3J 1P3, Canada
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2018年 / 41卷 / 09期
关键词：
TIME-VARYING DELAY; VARIABLE-STRUCTURE CONTROL; MARKOVIAN JUMP SYSTEMS; RIGID SPACECRAFT; TRACKING CONTROL; FLEXIBLE SPACECRAFT; BOUNDED DISTURBANCES; ACTUATOR SATURATION; LINEAR-SYSTEMS; ROBUST;
D O I：
10.2514/1.G003555
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：2041 / 2053
页数：13
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