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

^*Corresponding author for this work

Harbin Institute of Technology

Research output: Contribution to journal › Article › peer-review

4 Scopus citations

Abstract

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.

Original language	English
Pages (from-to)	1378-1383
Number of pages	6
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	22
Issue number	8
State	Published - Aug 2007
Externally published	Yes

Keywords

Aero-engine
Aerospace propulsion system
Linear matrix inequalities (LMI)
Performance
Pole placement
Switched linear systems

Cite this

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title = "Design of aero engine multi-loop controllers with switching characteristics",

abstract = "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.",

keywords = "Aero-engine, Aerospace propulsion system, Linear matrix inequalities (LMI), Performance, Pole placement, Switched linear systems",

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AU - Yu, Da Ren

AU - Liu, Xiao Feng

AU - Sui, Yan Feng

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N2 - 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.

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.

KW - Aero-engine

KW - Aerospace propulsion system

KW - Linear matrix inequalities (LMI)

KW - Performance

KW - Pole placement

KW - Switched linear systems

UR - https://www.scopus.com/pages/publications/34548515298

M3 - 文章

AN - SCOPUS:34548515298

SN - 1000-8055

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JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 8

ER -

Design of aero engine multi-loop controllers with switching characteristics

Abstract

Keywords

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