DocumentCode
2909319
Title
Fault detection using nonlinear parameter estimation
Author
Törnqvist, David ; Saha, Saikat ; Gustafsson, Fredrik
Author_Institution
Dept. of Electr. Eng., Linkoping Univ., Linköping, Sweden
fYear
2011
fDate
5-12 March 2011
Firstpage
1
Lastpage
6
Abstract
For linear and Gaussian systems, fault detection over a batch of data is well-studied, and analytical solutions exist in a stochastic framework. The parity space approach handles additive faults and can be shown to be equivalent to estimating the state trajectory and then removing its influence on the output sequence. Multiplicative faults in linear systems can be handled using parameter estimation methods, such as the EM-algorithm in combination with the Kalman smoother. For nonlinear and non-Gaussian systems, we propose to estimate the state trajectory and the faults over the data batch using a particle smoother and the EM-algorithm. The result is a generic fault detection and isolation scheme that applies to arbitrary nonlinear and non-Gaussian systems, where the faults are monitored over a sliding window.
Keywords
aircraft; fault diagnosis; parameter estimation; smoothing methods; EM-algorithm; Gaussian systems; Kalman smoother; aircraft subsystems; fault detection; fault diagnosis; generic fault detection; linear systems; multiplicative faults; nonlinear parameter estimation; parameter estimation methods; state trajectory; Atmospheric measurements; Fault detection; Kalman filters; Maximum likelihood estimation; Noise; Parameter estimation; Particle measurements;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2011 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-7350-2
Type
conf
DOI
10.1109/AERO.2011.5747438
Filename
5747438
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