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A Reusable and Adaptable Software Architecture for Embedded Space Flight System: The Core Flight Software System (CFS)The contents include the following: High availability. Hardware is in harsh environment. Flight processor (constraints) very widely due to power and weight constraints. Software must be remotely modifiable and still operate while changes are being made. Many custom one of kind interfaces for one of a kind missions. Sustaining engineering. Price of failure is high, tens to hundreds of millions of dollars.
Document ID
20050245086
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Wilmot, Jonathan
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Computer Operations And Hardware
Meeting Information
Meeting: International Conference on Hardware/Software Codesign and System Synthesis
Location: Jersey City, NJ
Country: United States
Start Date: September 18, 2005
End Date: September 21, 2005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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