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What Can Formal Methods Offer to Digital Flight Control Systems Design?Formal methods research is beginning to produce methods which will enable mathematical modeling of the physical behavior of digital hardware and software systems. The development of these methods directly supports the NASA mission of increasing the scope and effectiveness of flight system modeling capabilities.

The conventional, continuous mathematics that is used extensively in modeling flight systems is not adequate for accurate modeling of digital systems. Therefore, the current practice of digital flight control system design has not had the benefits of extensive mathematical modeling which are common in other parts of flight system engineering.

Formal methods research is showing that by using discrete mathematics, very accurate modeling of digital systems is possible. These discrete modeling methods are still in an embryonic stage. But when they are fully developed, they will bring the traditional benefits of modeling to digital hardware and software design. Sound reasoning about accurate mathematical models of flight control systems can be an important part of reducing the risks of unsafe flight control.
Document ID
19910008253
Acquisition Source
Legacy CDMS
Document Type
Presentation
Authors
Donald I Good
(Computational Logic Austin, Texas, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1990
Publication Information
Publication: NASA Formal Methods Workshop, 1990
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Stability and Control
Report/Patent Number
NASA-CP-10052
Meeting Information
Meeting: NASA Formal Methods Workshop
Location: Hampton, VA
Country: US
Start Date: August 20, 1990
End Date: August 23, 1990
Sponsors: National Aeronautics and Space Administration
Accession Number
91N17566
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
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