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Multi-disciplinary optimisation of distributed aero-engine control system architectures

机译:分布式航空发动机控制系统架构的多学科优化

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摘要

In aerospace, adoption of a distributed control strategy has many advantages such as: fewer and shorter buses, intrinsic partitioning, smaller control box size, increased health monitoring, increased system flexiblity and reduced vulnerability to hzardous events. However, this has to be traded off against the problems of greater complexity, processor diversity, accessibility, exposure of electronics to severe environments, power distribution, software production costs and management. This paper dsicusses the application of multi-disciplinary multi-objective optimisation to military gas turbine engine controller architecture design.
机译:在航空航天中,采用分布式控制策略具有许多优势,例如:总线越来越少,内部分区,控制箱尺寸更小,运行状况监控增加,系统灵活性更高以及对危险事件的脆弱性降低。但是,这必须权衡更大的复杂性,处理器多样性,可访问性,电子设备在恶劣环境中的使用,配电,软件生产成本和管理等问题。本文论述了多学科多目标优化技术在军用燃气轮机控制器结构设计中的应用。

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