Fault tolerant attitude control for spacecraft based on adaptive fast terminal sliding mode

被引：3
|
作者：
Zhao, Lin [1 ]
Yan, Xin [1 ]
Gao, Shuai-He [1 ]
机构：
[1] College of Automation, Harbin Engineering University, Harbin 150001, China
来源：
Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics | 2012年 / 34卷 / 05期
关键词：
Adaptive Control - Adaptive control methods - Fast terminal sliding mode controls - Fault tolerant control - Fault tolerant controllers - Finite time stability - Sliding mode surface - Terminal sliding mode;
D O I：
10.3969/j.issn.1001-506X.2012.05.23
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：982 / 988
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