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
Link To Document :
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