Design and simulation of control systems with actuators of aeroengine

Tie Jun Zheng; Xi Wang; Dao Liang Tan; Qi Han Li

Design and simulation of control systems with actuators of aeroengine

Tie Jun Zheng^*
, Xi Wang
, Dao Liang Tan
, Qi Han Li

^*此作品的通讯作者

能源与动力工程学院

Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

The influence of actuators on the dynamic performance of aeroengine control systems, and the intermediate state control systems design problem for certain model of aeroengine based on multivariable H_∞ controller design theory was investigated. The comparative simulation results were provided on the platform of numerical simulation for control systems with and without actuators, which demonstrate that actuators can help controller constrain control energy and in the incremental direction of control signal, system considered possesses strong robust stability and performance.

源语言	英语
页（从-至）	335-338
页数	4
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	26
期	4
出版状态	已出版 - 8月 2005

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title = "Design and simulation of control systems with actuators of aeroengine",

abstract = "The influence of actuators on the dynamic performance of aeroengine control systems, and the intermediate state control systems design problem for certain model of aeroengine based on multivariable H∞ controller design theory was investigated. The comparative simulation results were provided on the platform of numerical simulation for control systems with and without actuators, which demonstrate that actuators can help controller constrain control energy and in the incremental direction of control signal, system considered possesses strong robust stability and performance.",

keywords = "Aircraft engine, Control system, Numerical simulation, Robust control",

author = "Zheng, \{Tie Jun\} and Xi Wang and Tan, \{Dao Liang\} and Li, \{Qi Han\}",

year = "2005",

month = aug,

language = "英语",

volume = "26",

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

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AU - Zheng, Tie Jun

AU - Wang, Xi

AU - Tan, Dao Liang

AU - Li, Qi Han

PY - 2005/8

Y1 - 2005/8

N2 - The influence of actuators on the dynamic performance of aeroengine control systems, and the intermediate state control systems design problem for certain model of aeroengine based on multivariable H∞ controller design theory was investigated. The comparative simulation results were provided on the platform of numerical simulation for control systems with and without actuators, which demonstrate that actuators can help controller constrain control energy and in the incremental direction of control signal, system considered possesses strong robust stability and performance.

AB - The influence of actuators on the dynamic performance of aeroengine control systems, and the intermediate state control systems design problem for certain model of aeroengine based on multivariable H∞ controller design theory was investigated. The comparative simulation results were provided on the platform of numerical simulation for control systems with and without actuators, which demonstrate that actuators can help controller constrain control energy and in the incremental direction of control signal, system considered possesses strong robust stability and performance.

KW - Aircraft engine

KW - Control system

KW - Numerical simulation

KW - Robust control

UR - https://www.scopus.com/pages/publications/24744466968

M3 - 文章

AN - SCOPUS:24744466968

SN - 1001-4055

VL - 26

SP - 335

EP - 338

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 4

ER -

Design and simulation of control systems with actuators of aeroengine

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