The desirability and feasibility of computer-augmented support for the pre-implementation activities occurring during the development of flight control software was investigated. The specific topics to be investigated were the capabilities to be included in a pre-implementation support system for flight control software system development, and the specification of a preliminary design for such a system. Further, the pre-implementation support system was to be characterized and specified under the constraints that it: (1) support both description and assessment of flight control software requirements definitions and design specification; (2) account for known software description and assessment techniques; (3) be compatible with existing and planned NASA flight control software development support system; and (4) does not impose, but may encourage, specific development technologies. An overview of the results is given.


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    Title :

    Flight software requirements and design support system


    Contributors:
    Riddle, W. E. (author) / Edwards, B. (author)

    Publication date :

    1980-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English