论文信息 - Architectural Design of Distributed Control Systems for Aero Gas Turbine Engines Using Genetic Algorithms

Architectural Design of Distributed Control Systems for Aero Gas Turbine Engines Using Genetic Algorithms

This work presents a method for the design of distributed control systems for large civil jet engines using a genetic algorithm. The algorithm evaluates solutions based on three evaluation functions designed to ensure the proposed systems are both technically and commercially viable.

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