Stewart, Paul, Fleming, P. J. and MacKenzie, S. A. (2002) On the response surface methodology and designed experiments for computationally intensive distributed aerospace simulations. In: 2002 Winter Simulation conference, 8-11 December 2002, Hyatt Regency Hotel, San Diego, California, USA.
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Item Type: | Conference or Workshop contribution (Paper) |
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Item Status: | Live Archive |
Abstract
Distributed real-time simulation is the focus of intense development with complex systems being represented by individual component simulations interacting as a coherent model. Commercial off the shelf (COTS) and Freeware real-time software exists to provide data communication channels between he components subject to adequate system bandwidth. However, if the individual models are too computationally intensive to run in real-time, then the performance of the real-time simulation architecture is compromised.
In this paper, model representations are developed from dynamic simulation by the Response surface Methodology, allowing complex systems to be included in a real-time environment. A Permanent Magnet AC motor drive simulation with model reference control for a more electric aircraft application is examined as a candidate for inclusion in a realtime simulation environment.
Additional Information: | Distributed real-time simulation is the focus of intense development with complex systems being represented by individual component simulations interacting as a coherent model. Commercial off the shelf (COTS) and Freeware real-time software exists to provide data communication channels between he components subject to adequate system bandwidth. However, if the individual models are too computationally intensive to run in real-time, then the performance of the real-time simulation architecture is compromised. In this paper, model representations are developed from dynamic simulation by the Response surface Methodology, allowing complex systems to be included in a real-time environment. A Permanent Magnet AC motor drive simulation with model reference control for a more electric aircraft application is examined as a candidate for inclusion in a realtime simulation environment. |
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Keywords: | Response Surfaces, Distributed simulation, Real-time Simulation |
Subjects: | H Engineering > H660 Control Systems G Mathematical and Computer Sciences > G520 Systems Design Methodologies H Engineering > H600 Electronic and Electrical Engineering H Engineering > H410 Aeronautical Engineering |
Divisions: | College of Science > School of Engineering |
ID Code: | 2195 |
Deposited On: | 02 Mar 2010 23:05 |
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