DocumentCode
1242196
Title
FDI for Aircraft Systems Using Stochastic Pooled-NARMAX Representations: Design and Assessment
Author
Dimogianopoulos, Dimitrios G. ; Hios, John D. ; Fassois, Spilios D.
Author_Institution
Dept. of Mech. Eng. & Aeronaut., Univ. of Patras, Patras, Greece
Volume
17
Issue
6
fYear
2009
Firstpage
1385
Lastpage
1397
Abstract
In this paper, two statistical schemes aiming at effective fault detection and isolation (FDI) for aircraft systems are introduced. They are based on novel stochastic pooled nonlinear autoregressive moving average with exogenous excitation representations that model the relationships among available aircraft signals, as well as statistical decision making. The first, or ldquodirect,rdquo scheme relates a pilot input to a measurable flight attitude via a two-stage pooled representation. The second, or ldquoindirect,rdquo scheme relates four attitude-dependent flight variables via a proper pooled representation. Both schemes achieve effective FDI operation inside an entire flight regime, under stochastic effects and uncertainty and under various operating or environmental conditions, at the price of increased computational effort during training. Their performance and robustness are assessed via many flights conducted with an aircraft simulator inside the considered flight regime, under different conditions and under faults of various types and magnitudes.
Keywords
aircraft control; autoregressive moving average processes; decision making; fault diagnosis; FDI; aircraft simulator; aircraft systems; fault detection; fault isolation; statistical decision making; statistical schemes; stochastic pooled nonlinear autoregressive moving average; stochastic pooled-NARMAX representations; two-stage pooled representation; Aircraft expert systems; decision making; fault diagnosis; identification; modeling; nonlinear systems; stochastic systems;
fLanguage
English
Journal_Title
Control Systems Technology, IEEE Transactions on
Publisher
ieee
ISSN
1063-6536
Type
jour
DOI
10.1109/TCST.2008.2005836
Filename
4815393
Link To Document