Usage of Fault Detection Isolation and Recovery (FDIR) in CxP Launch Operations
Author:
Affiliation:
1. NASA Kennedy Space Center
2. NASA Ames Research Center
3. Perot Systems
4. ASRC Aerospace Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-2181
Reference8 articles.
1. Additional objectives include providing a path for certification of the FDIR architecture along with assessing FDIR performance capability. Performance testing of the TEAMS real time tool, was performed at the vendor's location, and documented. These results were presented5at an earlier IEEE conference. The task will also provide implementation/deploymentoptionsforintegrationwithinLCS. Ares I-X TVC FFM
2. Functional Fault Modeling Conventions and Practices for Real-Time Fault Isolation
3. Pre-Launch Diagnostics for Launch Vehicles
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