TY - GEN
T1 - Fault detection and reconstruction for micro-satellite power subsystem based on PCA
AU - Lee, Bo
AU - Wang, Xinsheng
PY - 2010
Y1 - 2010
N2 - 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.
AB - 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.
UR - https://www.scopus.com/pages/publications/79952167568
U2 - 10.1109/ISSCAA.2010.5632201
DO - 10.1109/ISSCAA.2010.5632201
M3 - 会议稿件
AN - SCOPUS:79952167568
SN - 9781424460441
T3 - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
SP - 1169
EP - 1173
BT - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
T2 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010
Y2 - 8 June 2010 through 10 June 2010
ER -