A direct adaptive actuator failure compensation scheme for satellite attitude control systems

被引：28
|
作者：
Ma, Yajie [1 ]
Jiang, Bin [1 ]
Tao, Gang [1 ,3 ]
Cheng, Yuehua [2 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Acad Frontier Sci, Nanjing 210016, Peoples R China
[3] Univ Virginia, Dept Elect & Comp Engn, Charlottesville, VA USA
来源：
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | 2014年 / 228卷 / 04期
基金：
中国国家自然科学基金;
关键词：
adaptive compensation; actuator failure; Satellite attitude control; uncertainty; backstepping; FAULT-TOLERANT CONTROL; BACKSTEPPING CONTROL; NONLINEAR-SYSTEMS; STABILIZATION; WHEELS;
D O I：
10.1177/0954410013476191
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A new direct adaptive failure compensation approach is developed for satellite attitude control systems in the presence of uncertain failures of redundant actuators. The adaptive failure compensation controller is designed via a backstepping design, which can accommodate uncertainties in actuator failure time instants, values, and patterns. The failure uncertainties are estimated directly by adaptive laws and the adaptive satellite attitude control system with actuator failures is analyzed, to show its desired stability and asymptotic tracking properties. Finally, simulation results of a satellite attitude control system with redundant reaction wheels are presented to demonstrate the effectiveness of the proposed adaptive failure compensation scheme.
引用
收藏
页码：542 / 556
页数：15
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