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