DocumentCode :
2470098
Title :
A simulation method for POBIT fault detection using Stateflow
Author :
Shi, Junyou ; Lee, Haiwei
Author_Institution :
Sch. of Reliability & Syst. Eng., BeiHang Univ., Beijing, China
fYear :
2012
fDate :
23-25 May 2012
Firstpage :
1
Lastpage :
7
Abstract :
The application and development of BIT technique in aircraft embedded diagnosis and PHM(Prognostic and Health Management)design are analyzed. For the purposes of Power-on BIT (POBIT) detection-threshold determination and detection capability analysis, a simulation method for POBIT fault detection based on Stateflow is presented. In this paper, the Stateflow simulation principle of POBIT is analyzed, and the typical simulation elements of POBIT are determined, with the Stateflow simulation modes of those elements made. Based on this, an analysis process of POBIT Stateflow modeling and simulation is formed. A typical avionics module POBIT is taken as the case, with the POBIT Stateflow model built and the simulation analysis made, and the result shows that this method can realize dynamic simulation for POBIT and be used for fault detection-threshold and detection capability analysis.
Keywords :
aerospace simulation; aircraft testing; avionics; built-in self test; condition monitoring; digital simulation; embedded systems; fault diagnosis; PHM; POBIT Stateflow modeling; POBIT fault detection; Stateflow simulation principle; aircraft embedded diagnosis; avionics module POBIT; built-in test; detection capability analysis; power-on BIT detection-threshold determination; prognostic and health management design; simulation method; Power-on BIT; Stateflow; detection logic; fault detection; simulation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Prognostics and System Health Management (PHM), 2012 IEEE Conference on
Conference_Location :
Beijing
ISSN :
2166-563X
Print_ISBN :
978-1-4577-1909-7
Electronic_ISBN :
2166-563X
Type :
conf
DOI :
10.1109/PHM.2012.6228885
Filename :
6228885
Link To Document :
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