DocumentCode :
2004736
Title :
Anomaly detection of spacecraft based on least squares support vector machine
Author :
Xiong Long ; Ma Hao-Dong ; Fang Hong-Zheng ; Zou Ke-Xu ; Yi Da-Wei
Author_Institution :
Beijing Aerosp. Meas. & Control Corp., Beijing, China
fYear :
2011
fDate :
24-25 May 2011
Firstpage :
1
Lastpage :
6
Abstract :
Anomaly detection is to identify abnormal behaviors of a system. It plays an important role in Prognostics and System Health Management (PHM) which is applied to monitor spacecraft´s performance, detect faults, identify the root cause of the fault, and predict the remaining useful life (RUL) in order to increase safety and reduce downtime of spacecraft in-orbit. This paper proposes a method to detect anomaly of spacecraft in-orbit based on Least Squares Support Vector Machine (LS SVM), which has excellent learning, classification and generalization ability. The process is as follows: (1) Data Collection and Preprocessing. Data such as current, voltage, temperature, vibration and so on are acquired in spacecraft in orbit and preprocessed firstly after they are sent to remote measurement and control centers in the ground, including filtering out the noise and removing non-cutting signals. (2) Feature Extraction. Features which contain any combination of numerical and categorical values are extracted and identified from the sensors´ signals using statistical methods. (3) Feature Selection. Principal Component Analysis (PCA) is used to select a subset of features that provides a more informative, robust representation of the information contained in the data since PCA is generally effective for dimensionality reduction and data compression. (4) Anomaly Detection. LS-SVM is used to identify abnormal behaviors of spacecraft in-orbit. Meanwhile, the time when the anomaly was first noticed and the potential causes of the anomaly ranging from subsystem to system level are determined. Finally, experimental data from a spacecraft in-orbit are used to test the performance of the algorithm and the results show that the proposed method achieves perfect accuracy and efficiency in anomaly detection of spacecraft in-orbit.
Keywords :
aerospace computing; aircraft maintenance; condition monitoring; fault diagnosis; feature extraction; learning (artificial intelligence); least squares approximations; principal component analysis; space research; space vehicles; support vector machines; classification ability; control center; data collection; data preprocessing; fault detection; feature extraction; feature selection; generalization ability; learning ability; least squares support vector machine; principal component analysis; prognostics and system health management; remaining useful life; remote measurement; spacecraft anomaly detection; spacecraft in-orbit; spacecraft performance monitor; Decoding; Equations; Frequency modulation; Monitoring; Orbits; Space vehicles; Support vector machines; Anomaly detection; LS-SVM; Spacecraft in-orbit;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Prognostics and System Health Management Conference (PHM-Shenzhen), 2011
Conference_Location :
Shenzhen
Print_ISBN :
978-1-4244-7951-1
Electronic_ISBN :
978-1-4244-7949-8
Type :
conf
DOI :
10.1109/PHM.2011.5939470
Filename :
5939470
Link To Document :
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