Output feedback control of aero-engine multi-loops with pole placement approach

Da Ren Yu; Xiao Feng Liu; Yan Feng Sui

Output feedback control of aero-engine multi-loops with pole placement approach

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

^*Corresponding author for this work

School of Energy Science and Engineering

Harbin Institute of Technology

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

1 Scopus citations

Abstract

An approach was proposed which addressed the design of output feedback H_∞ controllers. It satisfies the multi-loops switching control system on the closed-loop pole location. Sufficient and necessary conditions for feasibility were derived for a general class of convex regions of the complex plane. These conditions were expressed in terms of linear matrix inequalities (LMIs). Simulation results show the approach is feasible.

Original language	English
Pages (from-to)	2022-2025
Number of pages	4
Journal	Xitong Fangzhen Xuebao / Journal of System Simulation
Volume	19
Issue number	9
State	Published - 5 May 2007

Keywords

Aero-engine
Linear matrix inequality
Pole placement
Switching control

Cite this

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title = "Output feedback control of aero-engine multi-loops with pole placement approach",

abstract = "An approach was proposed which addressed the design of output feedback H∞ controllers. It satisfies the multi-loops switching control system on the closed-loop pole location. Sufficient and necessary conditions for feasibility were derived for a general class of convex regions of the complex plane. These conditions were expressed in terms of linear matrix inequalities (LMIs). Simulation results show the approach is feasible.",

keywords = "Aero-engine, Linear matrix inequality, Pole placement, Switching control",

author = "Yu, \{Da Ren\} and Liu, \{Xiao Feng\} and Sui, \{Yan Feng\}",

year = "2007",

month = may,

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language = "英语",

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T1 - Output feedback control of aero-engine multi-loops with pole placement approach

AU - Yu, Da Ren

AU - Liu, Xiao Feng

AU - Sui, Yan Feng

PY - 2007/5/5

Y1 - 2007/5/5

N2 - An approach was proposed which addressed the design of output feedback H∞ controllers. It satisfies the multi-loops switching control system on the closed-loop pole location. Sufficient and necessary conditions for feasibility were derived for a general class of convex regions of the complex plane. These conditions were expressed in terms of linear matrix inequalities (LMIs). Simulation results show the approach is feasible.

AB - An approach was proposed which addressed the design of output feedback H∞ controllers. It satisfies the multi-loops switching control system on the closed-loop pole location. Sufficient and necessary conditions for feasibility were derived for a general class of convex regions of the complex plane. These conditions were expressed in terms of linear matrix inequalities (LMIs). Simulation results show the approach is feasible.

KW - Aero-engine

KW - Linear matrix inequality

KW - Pole placement

KW - Switching control

UR - https://www.scopus.com/pages/publications/34248675504

M3 - 文章

AN - SCOPUS:34248675504

SN - 1004-731X

VL - 19

SP - 2022

EP - 2025

JO - Xitong Fangzhen Xuebao / Journal of System Simulation

JF - Xitong Fangzhen Xuebao / Journal of System Simulation

IS - 9

ER -

Output feedback control of aero-engine multi-loops with pole placement approach

Abstract

Keywords

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