Nonlinear attitude tracking control of underactuated three-inline tethered satellite

被引：0
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作者：
School of Astronautics, Harbin Institute of Technology, Harbin [1 ]
150001, China
机构：
来源：
Hangkong Xuebao | / 6卷 / 1995-2004期
关键词：
Attitude controller - Attitude tracking control - Bounded disturbances - Control saturation - Tethered satellite - Tethered satellite systems - Under-actuated systems - Uniformly ultimate boundedness;
D O I：
10.7527/S1000-6893.2014.0296
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学科分类号：
摘要：
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