DocumentCode :
3208346
Title :
Towards prognostics for electronics components
Author :
Saha, Bhaskar ; Celaya, Jose R. ; Wysocki, Philip F. ; Goebel, Kai F.
Author_Institution :
MCT, Inc, NASA Ames Res. Center, Moffett Field, CA
fYear :
2009
fDate :
7-14 March 2009
Firstpage :
1
Lastpage :
7
Abstract :
Electronics components have an increasingly critical role in avionics systems and in the development of future aircraft systems. Prognostics of such components is becoming a very important research field as a result of the need to provide aircraft systems with system level health management information. This paper focuses on a prognostics application for electronics components within avionics systems, and in particular its application to an Isolated Gate Bipolar Transistor (IGBT). This application utilizes the remaining useful life prediction, accomplished by employing the particle filter framework, leveraging data from accelerated aging tests on IGBTs. These tests induced thermal-electrical overstresses by applying thermal cycling to the IGBT devices. In-situ state monitoring, including measurements of steady-state voltages and currents, electrical transients, and thermal transients are recorded and used as potential precursors of failure.
Keywords :
aerospace components; aircraft; condition monitoring; insulated gate bipolar transistors; life testing; remaining life assessment; accelerated aging tests; aircraft system; avionics system; electrical transient; electronics components; health management system; isolated gate bipolar transistor; particle filter framework; remaining useful life prediction; thermal transient; Accelerated aging; Aerospace electronics; Aircraft; Bipolar transistors; Condition monitoring; Electronic components; Information management; Insulated gate bipolar transistors; Life testing; Particle filters;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace conference, 2009 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-2621-8
Electronic_ISBN :
978-1-4244-2622-5
Type :
conf
DOI :
10.1109/AERO.2009.4839676
Filename :
4839676
Link To Document :
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