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A high order approach to flight software development and testingThe use of a software development facility is discussed as a means of producing a reliable and maintainable ECS software system, and as a means of providing efficient use of the ECS hardware test facility. Principles applied to software design are given, including modularity, abstraction, hiding, and uniformity. The general objectives of each phase of the software life cycle are also given, including testing, maintenance, code development, and requirement specifications. Software development facility tools are summarized, and tool deficiencies recognized in the code development and testing phases are considered. Due to limited lab resources, the functional simulation capabilities may be indispensable in the testing phase.
Document ID
19820026573
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Steinbacher, J.
(Intermetrics, Inc. Huntington Beach, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1981
Subject Category
Computer Programming And Software
Report/Patent Number
AIAA PAPER 81-2150
Meeting Information
Meeting: In: Computers in Aerospace Conference
Location: San Diego, CA
Start Date: October 26, 1981
End Date: October 28, 1981
Accession Number
82A10108
Distribution Limits
Public
Copyright
Other

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