TY - GEN
T1 - A fault prognosis scheme based on SVM for the flight control system and PHM system
AU - Yin, W.
AU - Miao, W. S.
AU - Zhang, W. G.
PY - 2012
Y1 - 2012
N2 - Flight control system is a kind of complicated and various control system, in which some faults cannot be easy found. Moreover the fault trend is likewise not predictable. Using Support Vector Machines (SVMs), the faults not only are diagnosed but also are prognosed correctly. SVMs have originally been used for classification purposes but their principles can be extended easily to the task of regression and time series prediction. In this paper, the fault prognosis scheme of the flight control system was established through Support Vector Regression (SVR) in the solution follows from the fault detection scheme of the modern fighter plane. This scheme which consisted of the modules of the actuator, the steering face and fault diagnosis is discussed to overcome the problem of fault trend. It shows how to obtain weighted estimates for regression by applying SVM/SVR. The paper also discusses a framework combined SVM with HMM for the Prognostic and Health Management (PHM) of the flight control system. This method of this paper is illustrated for non-stability fault signals and demonstrates how to obtain predicted estimates with selection of an appropriate HMM units, in the case of future PHM design.
AB - Flight control system is a kind of complicated and various control system, in which some faults cannot be easy found. Moreover the fault trend is likewise not predictable. Using Support Vector Machines (SVMs), the faults not only are diagnosed but also are prognosed correctly. SVMs have originally been used for classification purposes but their principles can be extended easily to the task of regression and time series prediction. In this paper, the fault prognosis scheme of the flight control system was established through Support Vector Regression (SVR) in the solution follows from the fault detection scheme of the modern fighter plane. This scheme which consisted of the modules of the actuator, the steering face and fault diagnosis is discussed to overcome the problem of fault trend. It shows how to obtain weighted estimates for regression by applying SVM/SVR. The paper also discusses a framework combined SVM with HMM for the Prognostic and Health Management (PHM) of the flight control system. This method of this paper is illustrated for non-stability fault signals and demonstrates how to obtain predicted estimates with selection of an appropriate HMM units, in the case of future PHM design.
KW - component
KW - flight control system
KW - prognosis
KW - prognostic and health management
KW - Support vector machines
UR - https://www.scopus.com/pages/publications/84865752741
U2 - 10.1049/cp.2012.0514
DO - 10.1049/cp.2012.0514
M3 - 会议稿件
AN - SCOPUS:84865752741
SN - 9781849195386
T3 - IET Conference Publications
BT - 2012 International Conference on System Simulation, ICUSS 2012
T2 - 2012 International Conference on System Simulation, ICUSS 2012
Y2 - 6 April 2012 through 9 April 2012
ER -