DocumentCode
3575763
Title
Robust learning observer-based actuator fault reconstruction for satellite attitude control systems
Author
Qingxian Jia ; Huayi Li ; Xueqin Chen ; Yingchun Zhang
Author_Institution
Res. Center of Satellite Technol., Harbin Inst. of Technol. Harbin, Harbin, China
fYear
2014
Firstpage
556
Lastpage
560
Abstract
In this paper, robust actuator fault reconstruction for satellite attitude control systems (ACSs) in the presence of space environmental disturbances and actuator faults is investigated via a learning observer (LO). First, a nonlinear mathematical model of the satellite ACS satisfying Lipschitz constraint is established; then an LO is constructed to achieve robust reconstruction of satellite attitude angles, attitude angler velocities and actuator faults at the same time. Further, sufficient conditions for the robust stability of the LO are explicitly provided in this paper. The design problem of the proposed LO is formulated into a convex optimization problem in terms of linear matrix inequalities (LMIs) that can be directly solved using the LMI toolbox of MATLAB. At last, simulation studies on a satellite example are performed to illustrate the effectiveness and applicability of the presented LO-based fault-reconstructing strategy.
Keywords
artificial satellites; attitude control; convex programming; linear matrix inequalities; observers; robust control; ACS; LMI toolbox; LO; Lipschitz constraint; MATLAB; attitude angler velocities; convex optimization problem; learning observer-based actuator fault reconstruction; linear matrix inequalities; nonlinear mathematical model; robust actuator fault reconstruction; robust stability; satellite attitude angles; satellite attitude control systems; space environmental disturbances; sufficient conditions; Actuators; Attitude control; MATLAB; Mathematical model; Observers; Robustness; Satellites;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Control (ICMC), 2014 International Conference on
Print_ISBN
978-1-4799-2537-7
Type
conf
DOI
10.1109/ICMC.2014.7231617
Filename
7231617
Link To Document