Abstract The complexity of modern systems requires a holistic approach to modeling and simulation during the design phases. This often includes an integrated model of the overall system (architecture, function, and environment) as well as a link-up of computer-aided design tools, because there are many occasions in which there are aspects of the system that cannot be described in one tool. The paper introduces a converter program that bridges the gap between a CAD tool and a system design tool. Non-functional information that is relevant for the simulation is extracted from the three-dimensional CAD model and automatically inserted into the behavioral model of the system design tool. The latter is used for performance evaluation and indirect design optimization.
Optimization of avionic system architectures
CEAS Aeronautical Journal ; 2 , 1 ; 289-294
2011-08-20
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Optimization of avionic system architectures
Online Contents | 2011
|Tema Archiv | 1989
|Colloquium on Future Military Avionic Architectures
TIBKAT | 1990
Avionic Architectures for Space Exploration Missions
British Library Conference Proceedings | 2011
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