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Automated Propulsion Data Screening demonstration systemA fully-instrumented firing of a propulsion system typically generates a very large quantity of data. In the case of the Space Shuttle Main Engine (SSME), data analysis from ground tests and flights is currently a labor-intensive process. Human experts spend a great deal of time examining the large volume of sensor data generated by each engine firing. These experts look for any anomalies in the data which might indicate engine conditions warranting further investigation. The contract effort was to develop a 'first-cut' screening system for application to SSME engine firings that would identify the relatively small volume of data which is unusual or anomalous in some way. With such a system, limited and expensive human resources could focus on this small volume of unusual data for thorough analysis. The overall project objective was to develop a fully operational Automated Propulsion Data Screening (APDS) system with the capability of detecting significant trends and anomalies in transient and steady-state data. However, the effort limited screening of transient data to ground test data for throttle-down cases typical of the 3-g acceleration, and for engine throttling required to reach the maximum dynamic pressure limits imposed on the Space Shuttle. This APDS is based on neural networks designed to detect anomalies in propulsion system data that are not part of the data used for neural network training. The delivered system allows engineers to build their own screening sets for application to completed or planned firings of the SSME. ERC developers also built some generic screening sets that NASA engineers could apply immediately to their data analysis efforts.
Document ID
19950023163
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hoyt, W. Andes
(Engineering Research and Consulting, Inc. Tullahoma, TN, United States)
Choate, Timothy D.
(Engineering Research and Consulting, Inc. Tullahoma, TN, United States)
Whitehead, Bruce A.
(Tennessee Univ. Space Inst., Tullahoma, TN., United States)
Date Acquired
September 6, 2013
Publication Date
May 8, 1995
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
ERC-R-94-082
NAS 1.26:196636
NASA-CR-196636
SBA-0474-93-2-00007
Accession Number
95N29584
Funding Number(s)
CONTRACT_GRANT: NAS8-39184
CONTRACT_GRANT: NAS8-39782
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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