DocumentCode
3479767
Title
Real-time fault detection of the Space Shuttle Main Engine
Author
Panossian, H.V. ; Kemp, V.R.
Author_Institution
Rockwell Int., Canoga Park, CA, USA
fYear
1991
fDate
11-13 Dec 1991
Firstpage
2609
Abstract
The authors present a real-time failure-detection algorithm that will soon be implemented on the Space Shuttle Main Engine, (SSME) on an online basis. It is referred to as the real-time failure control (RTFC) algorithm, and it entails signal-based limit and trend checking based on information from complex model-based estimates. Thus, the SSME digital transient model and the power balance model are used to provide the algorithm with precomputed initial values, expected values, and standard deviations that serve as baselines for nominal operation
Keywords
aerospace computing; aerospace engines; failure analysis; online operation; real-time systems; space vehicles; Space Shuttle Main Engine; digital transient model; expected values; fault detection; online algorithm; power balance model; real-time failure control algorithm; real-time failure-detection algorithm; standard deviations; Condition monitoring; Costs; Engines; Fault detection; Frequency; Real time systems; Redundancy; Safety; Space shuttles; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1991., Proceedings of the 30th IEEE Conference on
Conference_Location
Brighton
Print_ISBN
0-7803-0450-0
Type
conf
DOI
10.1109/CDC.1991.261822
Filename
261822
Link To Document