Abstract
The design of distributed control systems (DCSs) for large, civil gas turbine engines is an inherently difficult architectural challenge. To date, the majority of research into DCSs has focused on the contributing technologies and high temperature electronics rather than the architecture of the system itself. This paper proposes a method for the architectural design of distributed systems using a genetic algorithm to generate, evaluate and refine designs. The method is presented along with results proving the concept.
Original language | English |
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Title of host publication | 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 |
Publication status | Published - 1 Dec 2011 |
Event | 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 - San Diego, CA, United States Duration: 31 Jul 2011 → 3 Aug 2011 |
Conference
Conference | 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 |
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Country/Territory | United States |
City | San Diego, CA |
Period | 31/07/11 → 3/08/11 |
ASJC Scopus subject areas
- Energy Engineering and Power Technology
- Aerospace Engineering
- Control and Systems Engineering
- Electrical and Electronic Engineering
- Mechanical Engineering