A discrete event systems approach to discriminating intermittent from permanent faults

Almost all work on model-based diagnosis (MBD) potentially presumes faults are per- sistent and does not take intermittent faults (IFs) into account. Therefore, it is common for diag- nosis systems to misjudge IFs as permanent faults (PFs), which are the major cause of the problems of false alarms,...

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Published inChinese journal of aeronautics Vol. 27; no. 2; pp. 390 - 396
Main Authors Deng, Guanqian, Qiu, Jing, Liu, Guanjun, Lyu, Kehong
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.04.2014
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ISSN1000-9361
2588-9230
DOI10.1016/j.cja.2013.07.001

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Summary:Almost all work on model-based diagnosis (MBD) potentially presumes faults are per- sistent and does not take intermittent faults (IFs) into account. Therefore, it is common for diag- nosis systems to misjudge IFs as permanent faults (PFs), which are the major cause of the problems of false alarms, cannot duplication and no fault found in aircraft avionics. To address this problem, a new fault model which includes PFs and IFs is presented based on discrete event systems (DESs). Thereafter, an approach is given to discriminate between PFs and IFs by diagnosing the current fault. In this paper, the regulations of (PFs and IFs) fault evolution through fault and reset events along the traces of system are studied, and then label propagation function is modified to account for PFs and the dynamic behavior of IFs and diagnosability of PFs and IFs are defined. Finally, illustrative examples are presented to demonstrate the proposed approach, and the analysis results show the fault types can be discriminated within bounded delay if the system is diagnosable.
Bibliography:Almost all work on model-based diagnosis (MBD) potentially presumes faults are per- sistent and does not take intermittent faults (IFs) into account. Therefore, it is common for diag- nosis systems to misjudge IFs as permanent faults (PFs), which are the major cause of the problems of false alarms, cannot duplication and no fault found in aircraft avionics. To address this problem, a new fault model which includes PFs and IFs is presented based on discrete event systems (DESs). Thereafter, an approach is given to discriminate between PFs and IFs by diagnosing the current fault. In this paper, the regulations of (PFs and IFs) fault evolution through fault and reset events along the traces of system are studied, and then label propagation function is modified to account for PFs and the dynamic behavior of IFs and diagnosability of PFs and IFs are defined. Finally, illustrative examples are presented to demonstrate the proposed approach, and the analysis results show the fault types can be discriminated within bounded delay if the system is diagnosable.
Deng Guanqian, Qiu Jing , Liu Guanjun, Lyu Kehong( Laboratory of Science and Technology on Integrated Logistics Support, College of Mechatronics and Automation, National University of Defense Technology, Changsha 410073, China)
Diagnosability;Diagnoser;Discrete event systemsFault diagnosis;Intermittent faults;Permanent faults
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ISSN:1000-9361
2588-9230
DOI:10.1016/j.cja.2013.07.001