Title
Real-time hardware implementation of symbolic health monitoring for aircraft engine components
Abstract
Symbolic dynamics based fault detection and condition monitoring is a new research area that provides a new set of tools for data analysis, fault detection and investigation of the dynamical systems. The partitioning concept is used to obtain a finite number of non-overlapping segments for a low-dimensional representation of time series. This analysis method for fault progression can be constructed from observed data sequences. This paper presents hardware implementation of symbolic dynamic filtering technique for real-time health monitoring of aircraft engine components using piezoelectric sensors. The signal processing tools are implemented in a two-step procedure using MATLAB/Simulink. The Simulink implementation gives a direct code generation capability that enables the generated code to be executed on the microprocessor for real-time applications.
Year
DOI
Venue
2010
10.1109/ACC.2010.5531250
American Control Conference
Keywords
DocType
ISSN
aerospace components,aerospace engines,aircraft,condition monitoring,filtering theory,piezoelectric actuators,time series,matlab,simulink,aircraft engine component,direct code generation,fault detection,partitioning concept,piezoelectric sensor,real-time hardware,signal processing tool,symbolic dynamic filtering,symbolic dynamics,symbolic health monitoring,sensors,real time systems,engines,data analysis,compressors,code generation,data acquisition,signal processing,real time,hardware,dynamic system
Conference
0743-1619
ISBN
Citations 
PageRank 
978-1-4244-7426-4
1
0.43
References 
Authors
2
3
Name
Order
Citations
PageRank
Yasar, M.110.43
Purekar, A.210.43
Sheth, D.310.43