TY - JOUR
T1 - Parity Space-Based Fault Detection by Minimum Error Minimax Probability Machine ⋆
AU - Zhong, Maiying
AU - Song, Yang
AU - Xue, Ting
AU - Yang, Rui
AU - Li, Wenbo
N1 - Publisher Copyright:
© 2018
PY - 2018
Y1 - 2018
N2 - This paper deals with the problem of parity space-based fault detection (FD) for linear discrete time systems in the framework of minimum error minimax probability machine (MEMPM). Traditional parity space-based FD is usually difficult to achieve acceptable tradeoff between missed alarm rate (MAR) and false alarm rate (FAR) without the exact stochastic properties of unknown input. To solve this problem, this paper proposes a novel method of parity space-based FD by MEMPM. Firstly, the integrated design of parity space vector, threshold, MAR and FAR is formulated as a problem of binary classification, i.e., the fault-free case and faulty case. By using the method of MEMPM, a bank of parity space vectors corresponding to different faulty scenarios and a threshold are then obtained, while an optimal trade-off between MAR and FAR is achieved in the worst-case setting. To show the effectiveness of proposed method, a satellite attitude control system subject to roll momentum wheel fault and pitch gyroscope fault is considered.
AB - This paper deals with the problem of parity space-based fault detection (FD) for linear discrete time systems in the framework of minimum error minimax probability machine (MEMPM). Traditional parity space-based FD is usually difficult to achieve acceptable tradeoff between missed alarm rate (MAR) and false alarm rate (FAR) without the exact stochastic properties of unknown input. To solve this problem, this paper proposes a novel method of parity space-based FD by MEMPM. Firstly, the integrated design of parity space vector, threshold, MAR and FAR is formulated as a problem of binary classification, i.e., the fault-free case and faulty case. By using the method of MEMPM, a bank of parity space vectors corresponding to different faulty scenarios and a threshold are then obtained, while an optimal trade-off between MAR and FAR is achieved in the worst-case setting. To show the effectiveness of proposed method, a satellite attitude control system subject to roll momentum wheel fault and pitch gyroscope fault is considered.
KW - Parity space
KW - false alarm rate
KW - fault detection
KW - minimum error minimax probability machine
KW - missed alarm rate
UR - http://www.scopus.com/inward/record.url?scp=85054594422&partnerID=8YFLogxK
U2 - 10.1016/j.ifacol.2018.09.568
DO - 10.1016/j.ifacol.2018.09.568
M3 - Article
AN - SCOPUS:85054594422
SN - 2405-8963
VL - 51
SP - 1292
EP - 1297
JO - 10th IFAC Symposium on Fault Detection, Supervision and Safety for Technical Processes SAFEPROCESS 2018: Warsaw, Poland, 29-31 August 2018
JF - 10th IFAC Symposium on Fault Detection, Supervision and Safety for Technical Processes SAFEPROCESS 2018: Warsaw, Poland, 29-31 August 2018
IS - 24
ER -