DocumentCode
2588554
Title
Model-based adaptation of flight-critical systems
Author
Ray, Sumit ; Karsai, Gabor ; McNeill, Kevin M.
Author_Institution
BAE Syst., Johnson City, NY, USA
fYear
2009
fDate
23-29 Oct. 2009
Abstract
In this paper we describe our experience applying the Producible Adaptive Model-based Software (PAMS) technology to the development of safety critical flight control software. PAMS is based on the state of the art Model Integrated Computing (MIC) environment from Vanderbilt University and represents a highly evolvable model-based software development methodology and tool suite that is revolutionary in its ability to address software adaptation. In particular, PAMS is an adaptation framework that introduces support for model transformations, co-evolution of models and modeling tools, and self-adaptation of systems. Analogous to delayed binding in compiler technology, PAMS enables binding software updates statically at design-time, on a configuration basis at load-time, and dynamically at run-time. The focus of this paper will be the application of PAMS to designtime evolution.
Keywords
aerospace control; safety-critical software; software engineering; flight critical systems; model based adaptation; model based software development; model integrated computing environment; model transformation; producible adaptive model-based software; safety critical flight control software; software adaptation; Adaptation model; Adaptive control; Aerospace control; Aerospace safety; Delay systems; Microwave integrated circuits; Programmable control; Programming; Software safety; Software tools;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 2009. DASC '09. IEEE/AIAA 28th
Conference_Location
Orlando, FL
Print_ISBN
978-1-4244-4078-8
Type
conf
DOI
10.1109/DASC.2009.5347443
Filename
5347443
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