NASA NTRS · 20050245086
A Reusable and Adaptable Software Architecture for Embedded Space Flight System: The Core Flight Software System (CFS)
Abstract
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.
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Wilmot, Jonathan. 2005-01-01. A Reusable and Adaptable Software Architecture for Embedded Space Flight System: The Core Flight Software System (CFS). https://ntrs.nasa.gov/citations/20050245086
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