DocumentCode
784121
Title
Fault estimation and accommodation for linear MIMO discrete-time systems
Author
Jiang, Bin ; Chowdhury, Fahmida N.
Author_Institution
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., China
Volume
13
Issue
3
fYear
2005
fDate
5/1/2005 12:00:00 AM
Firstpage
493
Lastpage
499
Abstract
In this brief, a methodology for detection and accommodation of actuator faults for a class of multi-input-multi-output (MIMO) stochastic systems is presented. First, a new real-time fault estimation module that estimates the actuator effectiveness is developed. The actuator fault diagnosis is based on the estimation of the state vector. Under some conditions, the stochastic system is transformed into two separate subsystems. One of them is not affected by actuator faults, so a reduced order Kalman filter can be used to estimate its states. The other, whose states are measurable, is affected by the faults. Then, the output of the nominal controller is reconfigured to compensate for the loss of actuator effectiveness in the system. Simulation results of a helicopter in vertical plane is presented to demonstrate the performance of the proposed fault-tolerant control scheme.
Keywords
Kalman filters; MIMO systems; aerospace control; discrete time systems; fault diagnosis; linear systems; reduced order systems; state estimation; stochastic systems; MIMO system; actuator fault diagnosis; discrete-time system; fault estimation; linear system; multi-input-multi-output stochastic system; nominal control; reduced order Kalman filter; state vector estimation; uncertain system; Actuators; Aerospace control; Control systems; Fault detection; Fault diagnosis; Fault tolerant systems; MIMO; Sensor systems; State estimation; Stochastic systems; Fault accommodation; fault estimation; flight control; linear stochastic systems; uncertainty;
fLanguage
English
Journal_Title
Control Systems Technology, IEEE Transactions on
Publisher
ieee
ISSN
1063-6536
Type
jour
DOI
10.1109/TCST.2004.839569
Filename
1424028
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