DocumentCode
2840398
Title
Design for validation [digital avionics]
Author
Johnson, Sally C. ; Butler, Ricky W.
Author_Institution
NASA Langley Res. Center, Hampton, VA, USA
fYear
1991
fDate
14-17 Oct 1991
Firstpage
487
Lastpage
492
Abstract
Outlines an approach for the development of ultrareliable digital avionics for civil air transports-a design-for-validation philosophy that includes rigorous application of formal methods. The basic concept of the methodology is introduced, and the role of formal methods is explored. System design begins with a detailed description of the system requirements written in a formal, mathematical language. The system design then proceeds in a hierarchical fashion from a highest-level specification of the system down to a detailed implementation level. Therefore, formal methods are applied to the total systems, not just to the individual subsystems, and all interactions between subsystems are formally described and understood. The impact of the design-for-validation philosophy on the system design process is demonstrated by two simple examples
Keywords
aircraft instrumentation; digital instrumentation; reliability; civil air transports; formal methods; highest-level specification; subsystems; ultrareliable digital avionics; Aerospace electronics; Application software; Certification; Computer aided analysis; Design methodology; Engines; Failure analysis; Hardware; NASA; Power system reliability;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1991. Proceedings., IEEE/AIAA 10th
Conference_Location
Los Angeles, CA
Type
conf
DOI
10.1109/DASC.1991.177214
Filename
177214
Link To Document