Design of aero engine multi-loop controllers with switching characteristics

Da Ren Yu; Xiao Feng Liu; Yan Feng Sui

Design of aero engine multi-loop controllers with switching characteristics

Da Ren Yu^*
, Xiao Feng Liu
, Yan Feng Sui

^*此作品的通讯作者

Harbin Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

4 引用（Scopus）

摘要

The switching problem of aero-engine multi-loops control system was studied, and the performance index requirements were also analyzed. Based on the pole placement and H_∞ robust synthesis, linear matrix inequalities (LMI) were constructed to provide a firm basis for determining H_∞, design method under multi-loop switching. As compared with traditional method of single-loop system, the simulation showed the feasibility and the necessity of the method hereto.

源语言	英语
页（从-至）	1378-1383
页数	6
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	22
期	8
出版状态	已出版 - 8月 2007
已对外发布	是

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引用此

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AB - The switching problem of aero-engine multi-loops control system was studied, and the performance index requirements were also analyzed. Based on the pole placement and H∞ robust synthesis, linear matrix inequalities (LMI) were constructed to provide a firm basis for determining H∞, design method under multi-loop switching. As compared with traditional method of single-loop system, the simulation showed the feasibility and the necessity of the method hereto.

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KW - Aerospace propulsion system

KW - Linear matrix inequalities (LMI)

KW - Performance

KW - Pole placement

KW - Switched linear systems

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Design of aero engine multi-loop controllers with switching characteristics

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