Robust H∞/PI state feedback control for aeroengine

Xi Wang; Nai Xiang Han; Xi Fa Li; Yun Hua Li

Robust H_∞/PI state feedback control for aeroengine

Xi Wang^*
, Nai Xiang Han
, Xi Fa Li
, Yun Hua Li

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University
First Inst. of Air Force

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

6 Scopus citations

Abstract

Considering the uncertainty model of aeroengine, the equivalent certainty system that quadratically stabilizes the plant can be obtained by restricting the H infinity norm of closed loop transform function from the disturbance input to the controlled output. A design method of robust H_∞/PI style controller was given by means of two free parameter in H_∞ state feedback controller subject to the constraints of PI structure. The robust performance was simulated on the SIMULINK environment.

Original language	English
Pages (from-to)	364-367
Number of pages	4
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	24
Issue number	4
State	Published - Aug 2003

Keywords

Aircraft engine
Controller
Flight control
State feedback

Cite this

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title = "Robust H∞/PI state feedback control for aeroengine",

abstract = "Considering the uncertainty model of aeroengine, the equivalent certainty system that quadratically stabilizes the plant can be obtained by restricting the H infinity norm of closed loop transform function from the disturbance input to the controlled output. A design method of robust H∞/PI style controller was given by means of two free parameter in H∞ state feedback controller subject to the constraints of PI structure. The robust performance was simulated on the SIMULINK environment.",

keywords = "Aircraft engine, Controller, Flight control, State feedback",

author = "Xi Wang and Han, \{Nai Xiang\} and Li, \{Xi Fa\} and Li, \{Yun Hua\}",

year = "2003",

month = aug,

language = "英语",

volume = "24",

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journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "China Aerospace Science and Industry Corp",

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T1 - Robust H∞/PI state feedback control for aeroengine

AU - Wang, Xi

AU - Han, Nai Xiang

AU - Li, Xi Fa

AU - Li, Yun Hua

PY - 2003/8

Y1 - 2003/8

N2 - Considering the uncertainty model of aeroengine, the equivalent certainty system that quadratically stabilizes the plant can be obtained by restricting the H infinity norm of closed loop transform function from the disturbance input to the controlled output. A design method of robust H∞/PI style controller was given by means of two free parameter in H∞ state feedback controller subject to the constraints of PI structure. The robust performance was simulated on the SIMULINK environment.

AB - Considering the uncertainty model of aeroengine, the equivalent certainty system that quadratically stabilizes the plant can be obtained by restricting the H infinity norm of closed loop transform function from the disturbance input to the controlled output. A design method of robust H∞/PI style controller was given by means of two free parameter in H∞ state feedback controller subject to the constraints of PI structure. The robust performance was simulated on the SIMULINK environment.

KW - Aircraft engine

KW - Controller

KW - Flight control

KW - State feedback

UR - https://www.scopus.com/pages/publications/0346148133

M3 - 文章

AN - SCOPUS:0346148133

SN - 1001-4055

VL - 24

SP - 364

EP - 367

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 4

ER -

Robust H_∞/PI state feedback control for aeroengine

Abstract

Keywords

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