The core Flight System (cFS) is a flight software (FSW) product line developed by the Flight Software Systems Branch (FSSB) at NASA's Goddard Space Flight Center (GSFC). The cFS uses compile-time configuration parameters to implement variable requirements to enable portability across embedded computing platforms and to implement different end-user functional needs. The verification and validation of these requirements is proving to be a significant challenge. This paper describes the challenges facing the cFS and the results of a pilot effort to apply EXB Solution's testing approach to the cFS applications.
Automated Test for NASA CFS
2015
13 pages
Report
Keine Angabe
Englisch
Computer Software , Applications programs (computers) , Automatic flight control , Software engineering , Software development tools , Configuration management , Independent variables , Performance tests , Program verification (computers) , Proving , User requirements , Software reuse , Cost analysis , Nasa programs
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