DocumentCode
3745754
Title
Fault Prediction for Satellite Attitude Control System Based on Fuzzy-Parity Equation and Grey Model
Author
Zhang Chunhua;Song Hua;Xiong Kai
Author_Institution
Sch. of Autom. Sci. &
fYear
2015
Firstpage
1879
Lastpage
1884
Abstract
Since present fault prediction method of satellite attitude control system cannot describe and predict the nonlinear system effectively, a new method based on fuzzy-parity equation and grey GM (1, 1) model is presented in this paper. Firstly, fuzzy-parity equation and Kalman filter are utilized to extract the fault feature of satellite actuator. Translation transformation and buffer operator are adopted to process the fault feature so as to establish an equal dimension and new information GM (1, 1) model. Then the development trend of the fault feature is predicted and the confidence level of one-step prediction result is evaluated through the prediction grey-level. Simulations demonstrate that the proposed method can predict fault trend effectively and accurately.
Keywords
"Mathematical model","Predictive models","Actuators","Satellites","Attitude control","Feature extraction"
Publisher
ieee
Conference_Titel
Instrumentation and Measurement, Computer, Communication and Control (IMCCC), 2015 Fifth International Conference on
Type
conf
DOI
10.1109/IMCCC.2015.399
Filename
7406181
Link To Document