DocumentCode
2440872
Title
Unsupervised Anomaly Detection and Diagnosis for Liquid Rocket Engine Propulsion
Author
Martin, Rodney A.
Author_Institution
NASA Ames Res. Center, Moffett Field
fYear
2007
fDate
3-10 March 2007
Firstpage
1
Lastpage
15
Abstract
The results of a comprehensive array of unsupervised anomaly detection algorithms applied to Space Shuttle main engine (SSME) data are presented. Most of the algorithms are based upon variants of the well-known unconditional Gaussian mixture model (GMM). One goal of the paper is to demonstrate the maximum utility of these algorithms by the exhaustive development of a very simple GMM. Selected variants will provide us with the added benefit of diagnostic capability. Another algorithm that shares a common technique for detection with the GMM is presented, but instead uses a different modeling paradigm. The model provides a more rich description of the dynamics of the data, however the data requirements are quite modest. We will show that this very simple and straightforward method finds an event that characterizes a departure from nominal operation. We show that further diagnostic investigation with the GMM-based method can be used as a means to gain insight into operational idiosyncrasies for this nominally categorized test. Therefore, by using both modeling paradigms we can corroborate planned operational commands or provide warnings for unexpected operational commands.
Keywords
Gaussian processes; condition monitoring; fault diagnosis; rocket engines; space vehicles; Space Shuttle main engine data; diagnostic investigation; liquid rocket engine propulsion; operational commands; unconditional Gaussian mixture model; unsupervised anomaly detection; Alarm systems; Costs; Detection algorithms; Engines; Extraterrestrial measurements; Fault detection; Performance analysis; Propulsion; Rockets; Space shuttles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2007 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
1-4244-0524-6
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2007.352949
Filename
4161687
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