Research of Model-based Aeroengine Control System Design Structure and Workflow

摘要：

　　The control system of aeroengine design is a complex system engineering containing many subsystems.To improve the efficiency of areoengine control system design and reduce the cost and development period of research procedure,model-based areoengine control system design method can be used for integrating systems,collaborative design and optimizing design.Model-based aeroengine control system design workflow consists of the phases from analysis of system requirements to semi-physics simulation verification.The management approach and design procedure can help to separate the whole design workflow into different sub-phases which can help to scheme the concurrent design procedure of complex control system in order to improve the efficiency of aeroengine design and optimize the performance of aeroengine control system.

关键词： Control system of Aeroengine Simulation Model-based,Simulation Design Structure

作者: Dong Zhang Jin-zhi Lu Lin Wang Jun Li

作者单位: AVIC,Shenyang Engine Design and Research Institute,China

会议类型: 国际会议

会议名称: 2014 Asia-Pacific International Symposium on Aerospace Technology(2014亚太航空航天技术学术会议)

会议地点: 上海

会议语种:英文

页码: 1-7

在线出版日期: 2014-09-24（万方平台首次上网日期，不代表论文的发表时间）