TY - GEN
T1 - Fault diagnosis of aircraft power supply based on Priority Dynamic Fault Tree
AU - Huang, Zhengting
AU - Wang, Zhongsheng
AU - Liu, Zhenbao
PY - 2012
Y1 - 2012
N2 - In this paper, we propose a novel fault diagnosis method for aircraft power supply system. We constructed the Dynamic Fault Tree (DFT) of the Constant Speed Constant Frequency Alternation Current (CSCF-AC) power supply system based on the Priority Dynamic Fault Tree (PDFT). And by adding a new temporal operator BEFORE (BF) to the usual Boolean operators, we derived the structure function of the top event. Then two laws were provided to reduce this structure function to a sum-of-product canonical form, where each product term defined a minimal cut set (MCS) or a minimal cut sequence set (MCSS) of this fault tree. This approach provides a complete qualitative description of the system without resorting to the corresponding Markov model. Then a 3-layer network diagnosis system was designed and realized for the fault diagnosis of aircraft power supply, including onboard layer, ground maintenance layer and remote expert layer. This 3-layer system enhances the flow of complex fault data into higher expert layer to realize the advanced diagnosis.
AB - In this paper, we propose a novel fault diagnosis method for aircraft power supply system. We constructed the Dynamic Fault Tree (DFT) of the Constant Speed Constant Frequency Alternation Current (CSCF-AC) power supply system based on the Priority Dynamic Fault Tree (PDFT). And by adding a new temporal operator BEFORE (BF) to the usual Boolean operators, we derived the structure function of the top event. Then two laws were provided to reduce this structure function to a sum-of-product canonical form, where each product term defined a minimal cut set (MCS) or a minimal cut sequence set (MCSS) of this fault tree. This approach provides a complete qualitative description of the system without resorting to the corresponding Markov model. Then a 3-layer network diagnosis system was designed and realized for the fault diagnosis of aircraft power supply, including onboard layer, ground maintenance layer and remote expert layer. This 3-layer system enhances the flow of complex fault data into higher expert layer to realize the advanced diagnosis.
KW - 3-layer network diagnosis system
KW - Aircraft power supply
KW - Fault diagnosis
KW - Priority dynamic fault tree
UR - http://www.scopus.com/inward/record.url?scp=84862936007&partnerID=8YFLogxK
U2 - 10.4028/www.scientific.net/AMR.443-444.229
DO - 10.4028/www.scientific.net/AMR.443-444.229
M3 - 会议稿件
AN - SCOPUS:84862936007
SN - 9783037852897
T3 - Advanced Materials Research
SP - 229
EP - 236
BT - Manufacturing Science and Materials Engineering
T2 - 2010 International Conference on Manufacturing Science and Materials Engineering, ICMSME 2011
Y2 - 14 October 2011 through 15 October 2011
ER -