Functional Fault Modeling of a Cryogenic System for Real-Time Fault Detection and IsolationThe purpose of this paper is to present the model development process used to create a Functional Fault Model (FFM) of a liquid hydrogen (L H2) system that will be used for realtime fault isolation in a Fault Detection, Isolation and Recover (FDIR) system. The paper explains th e steps in the model development process and the data products required at each step, including examples of how the steps were performed fo r the LH2 system. It also shows the relationship between the FDIR req uirements and steps in the model development process. The paper concl udes with a description of a demonstration of the LH2 model developed using the process and future steps for integrating the model in a live operational environment.
Document ID
20110005477
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Ferrell, Bob (NASA Kennedy Space Center Cocoa Beach, FL, United States)
Lewis, Mark (NASA Kennedy Space Center Cocoa Beach, FL, United States)
Perotti, Jose (NASA Kennedy Space Center Cocoa Beach, FL, United States)
Oostdyk, Rebecca (ASRC Aerospace Corp. Cocoa Beach, FL, United States)
Brown, Barbara (NASA Ames Research Center Moffett Field, CA, United States)