DocumentCode :
3025969
Title :
Fault detection and reconstruction for micro-satellite power subsystem based on PCA
Author :
Lee, Bo ; Wang, Xinsheng
Author_Institution :
Sch. of Astronaut., BeiHang Univ., Beijing, China
fYear :
2010
fDate :
8-10 June 2010
Firstpage :
1169
Lastpage :
1173
Abstract :
Fault detection and reconstruction for micro-satellite power subsystem was achieved by using the principal component analysis (PCA) method. Four typical kinds of sensor failure were identified. The principle to establish the PCA model, diagnose and reconstruct faulty sensors was presented. A model of a satellite´s power subsystem, which is consisted of voltage, temperature, and current parameters, was introduced. Using the normal data acquired from the experiment, we established the approximate PCA model for the satellite power system. With the incorrect data introduced to simulate the sensor failure occurrence, the value of squared prediction error (SPE) and sensor validity index (SVI) was detected beyond the confidence limit. Subsequently, the faulty sensor was isolated and reconstructed. The simulation results indicated that the PCA method was probably effective for fault detection and reconstruction in satellite power subsystem.
Keywords :
artificial satellites; power supplies to apparatus; principal component analysis; PCA; fault detection; fault reconstruction; micro-satellite power subsystem; principal component analysis; satellite power system; sensor failure; sensor validity index; squared prediction error; Accuracy; Computational modeling; Data models; Fault detection; Fault diagnosis; Principal component analysis; Satellites;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-6043-4
Electronic_ISBN :
978-1-4244-7505-6
Type :
conf
DOI :
10.1109/ISSCAA.2010.5632201
Filename :
5632201
Link To Document :
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