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Lessons Learned on Implementing Fault Detection, Isolation, and Recovery (FDIR) in a Ground Launch EnvironmentThis paper's main purpose is to detail issues and lessons learned regarding designing, integrating, and implementing Fault Detection Isolation and Recovery (FDIR) for Constellation Exploration Program (CxP) Ground Operations at Kennedy Space Center (KSC). Part of the0 overall implementation of National Aeronautics and Space Administration's (NASA's) CxP, FDIR is being implemented in three main components of the program (Ares, Orion, and Ground Operations/Processing). While not initially part of the design baseline for the CxP Ground Operations, NASA felt that FDIR is important enough to develop, that NASA's Exploration Systems Mission Directorate's (ESMD's) Exploration Technology Development Program (ETDP) initiated a task for it under their Integrated System Health Management (ISHM) research area. This task, referred to as the FDIIR project, is a multi-year multi-center effort. The primary purpose of the FDIR project is to develop a prototype and pathway upon which Fault Detection and Isolation (FDI) may be transitioned into the Ground Operations baseline. Currently, Qualtech Systems Inc (QSI) Commercial Off The Shelf (COTS) software products Testability Engineering and Maintenance System (TEAMS) Designer and TEAMS RDS/RT are being utilized in the implementation of FDI within the FDIR project. The TEAMS Designer COTS software product is being utilized to model the system with Functional Fault Models (FFMs). A limited set of systems in Ground Operations are being modeled by the FDIR project, and the entire Ares Launch Vehicle is being modeled under the Functional Fault Analysis (FFA) project at Marshall Space Flight Center (MSFC). Integration of the Ares FFMs and the Ground Processing FFMs is being done under the FDIR project also utilizing the TEAMS Designer COTS software product. One of the most significant challenges related to integration is to ensure that FFMs developed by different organizations can be integrated easily and without errors. Software Interface Control Documents (ICDs) for the FFMs and their usage will be addressed as the solution to this issue. In particular, the advantages and disadvantages of these ICDs across physically separate development groups will be delineated.
Document ID
20130012528
Acquisition Source
Kennedy Space Center
Document Type
Other
Authors
Ferrell, Bob A.
(NASA Kennedy Space Center Lompoc, CA, United States)
Lewis, Mark E.
(NASA Kennedy Space Center Lompoc, CA, United States)
Perotti, Jose M.
(NASA Kennedy Space Center Lompoc, CA, United States)
Brown, Barbara L.
(NASA Kennedy Space Center Lompoc, CA, United States)
Oostdyk, Rebecca L.
(ASRC Aerospace Corp. Cocoa Beach, FL, United States)
Goetz, Jesse W.
(ASRC Aerospace Corp. Cocoa Beach, FL, United States)
Date Acquired
August 27, 2013
Publication Date
January 1, 2010
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
KSC-2009-271
Report Number: KSC-2009-271
Distribution Limits
Public
Copyright
Public Use Permitted.
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