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Integrated System Health Management (ISHM) for Test Stand and J-2X Engine: Core ImplementationISHM capability enables a system to detect anomalies, determine causes and effects, predict future anomalies, and provides an integrated awareness of the health of the system to users (operators, customers, management, etc.). NASA Stennis Space Center, NASA Ames Research Center, and Pratt & Whitney Rocketdyne have implemented a core ISHM capability that encompasses the A1 Test Stand and the J-2X Engine. The implementation incorporates all aspects of ISHM; from anomaly detection (e.g. leaks) to root-cause-analysis based on failure mode and effects analysis (FMEA), to a user interface for an integrated visualization of the health of the system (Test Stand and Engine). The implementation provides a low functional capability level (FCL) in that it is populated with few algorithms and approaches for anomaly detection, and root-cause trees from a limited FMEA effort. However, it is a demonstration of a credible ISHM capability, and it is inherently designed for continuous and systematic augmentation of the capability. The ISHM capability is grounded on an integrating software environment used to create an ISHM model of the system. The ISHM model follows an object-oriented approach: includes all elements of the system (from schematics) and provides for compartmentalized storage of information associated with each element. For instance, a sensor object contains a transducer electronic data sheet (TEDS) with information that might be used by algorithms and approaches for anomaly detection, diagnostics, etc. Similarly, a component, such as a tank, contains a Component Electronic Data Sheet (CEDS). Each element also includes a Health Electronic Data Sheet (HEDS) that contains health-related information such as anomalies and health state. Some practical aspects of the implementation include: (1) near real-time data flow from the test stand data acquisition system through the ISHM model, for near real-time detection of anomalies and diagnostics, (2) insertion of the J-2X predictive model providing predicted sensor values for comparison with measured values and use in anomaly detection and diagnostics, and (3) insertion of third-party anomaly detection algorithms into the integrated ISHM model.
Document ID
20080015891
Acquisition Source
Stennis Space Center
Document Type
Conference Paper
Authors
Figueroa, Jorge F.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Schmalzel, John L.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Aguilar, Robert
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Shwabacher, Mark
(NASA Ames Research Center Moffett Field, CA, United States)
Morris, Jon
(Jacobs Technology United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2008
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
SSTI-2200-0092
Meeting Information
Meeting: 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Location: Hartford, CT
Country: United States
Start Date: July 20, 2008
End Date: July 23, 2008
Sponsors: American Society of Mechanical Engineers, American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS13-02014
CONTRACT_GRANT: NNS04AB67T
Distribution Limits
Public
Copyright
Public Use Permitted.
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