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Space Station Freedom integrated fault modelA demonstration of an integrated fault propagation model for Space Station Freedom is described. The demonstration uses a HyperCard graphical interface to show how failures can propagate from one component to another, both within a system and between systems. It also shows how hardware failures can impact certain defined functions like reboost, atmosphere maintenance or collision avoidance. The demonstration enables the user to view block diagrams for the various space station systems using an overview screen, and interactively choose a component and see what single or dual failure combinations can cause it to fail. It also allows the user to directly view the fault model, which is a collection of drawing and text listings accessible from a guide screen. Fault modeling provides a useful technique for analyzing individual systems and also interactions between systems in the presence of multiple failures so that a complete picture of failure tolerance and component criticality can be achieved.
Document ID
19900011357
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Becker, Fred J.
(Lockheed Engineering and Sciences Co. Houston, TX, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1989
Publication Information
Publication: NASA, Lyndon B. Johnson Space Center, Graphics Technology in Space Applications (GTSA 1989)
Subject Category
Computer Programming And Software
Accession Number
90N20673
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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