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
International Test and Evaluation Symposium ; 2015 ; Arlington, VA, United States
2015-08-18
Conference paper
No indication
English
British Library Conference Proceedings | 2015
|NTIS | 2015
|NTRS | 1986
|NTRS | 2017
|NTIS | 2017
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