Analysis of the characteristics by modeling and simulation of actuator in flight control system

Xiao Hu; Zhenjie Mao; Zongxia Jiao; Shuai Wu; Xiao Yu; Fengyu Li

doi:10.1109/CGNCC.2014.7007581

Analysis of the characteristics by modeling and simulation of actuator in flight control system

Xiao Hu
, Zhenjie Mao
, Zongxia Jiao
, Shuai Wu^*
, Xiao Yu
, Fengyu Li

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University
Aviation Industry Development Research Center of China

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

8 Scopus citations

Abstract

Flight control system consists of flight controller, sensor, and actuator. Currently, the research focuses on the design and optimization of flight controller, regardless the influence of actuator. This paper is devoted to find out the way actuator effects the flight control system in both dynamic and energy consumption by substituting actuator (hydraulic actuator and electro-hydrostatic actuator) model into the model of flight control system. Results revealed that the model with electro-hydrostatic actuator is better than another in energy consumption characteristics, but worse in dynamic characteristics.

Original language	English
Title of host publication	2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	2618-2623
Number of pages	6
ISBN (Electronic)	9781479946990
DOIs	https://doi.org/10.1109/CGNCC.2014.7007581
State	Published - 12 Jan 2015
Event	6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 - Yantai, China Duration: 8 Aug 2014 → 10 Aug 2014

Publication series

Name	2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

Conference

Conference	6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
Country/Territory	China
City	Yantai
Period	8/08/14 → 10/08/14

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

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10.1109/CGNCC.2014.7007581

Cite this

Hu, X., Mao, Z., Jiao, Z., Wu, S., Yu, X., & Li, F. (2015). Analysis of the characteristics by modeling and simulation of actuator in flight control system. In 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 (pp. 2618-2623). Article 7007581 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2014.7007581

Hu, Xiao ; Mao, Zhenjie ; Jiao, Zongxia et al. / Analysis of the characteristics by modeling and simulation of actuator in flight control system. 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc., 2015. pp. 2618-2623 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014).

@inproceedings{aea3c03135a14c50b478ee63b499b773,

title = "Analysis of the characteristics by modeling and simulation of actuator in flight control system",

abstract = "Flight control system consists of flight controller, sensor, and actuator. Currently, the research focuses on the design and optimization of flight controller, regardless the influence of actuator. This paper is devoted to find out the way actuator effects the flight control system in both dynamic and energy consumption by substituting actuator (hydraulic actuator and electro-hydrostatic actuator) model into the model of flight control system. Results revealed that the model with electro-hydrostatic actuator is better than another in energy consumption characteristics, but worse in dynamic characteristics.",

author = "Xiao Hu and Zhenjie Mao and Zongxia Jiao and Shuai Wu and Xiao Yu and Fengyu Li",

note = "Publisher Copyright: {\textcopyright} 2014 IEEE.; 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 ; Conference date: 08-08-2014 Through 10-08-2014",

year = "2015",

month = jan,

day = "12",

doi = "10.1109/CGNCC.2014.7007581",

language = "英语",

series = "2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "2618--2623",

booktitle = "2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014",

address = "美国",

}

Hu, X, Mao, Z, Jiao, Z , Wu, S, Yu, X & Li, F 2015, Analysis of the characteristics by modeling and simulation of actuator in flight control system. in 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014., 7007581, 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014, Institute of Electrical and Electronics Engineers Inc., pp. 2618-2623, 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014, Yantai, China, 8/08/14. https://doi.org/10.1109/CGNCC.2014.7007581

Analysis of the characteristics by modeling and simulation of actuator in flight control system. / Hu, Xiao; Mao, Zhenjie; Jiao, Zongxia et al.
2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc., 2015. p. 2618-2623 7007581 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Analysis of the characteristics by modeling and simulation of actuator in flight control system

AU - Hu, Xiao

AU - Mao, Zhenjie

AU - Jiao, Zongxia

AU - Wu, Shuai

AU - Yu, Xiao

AU - Li, Fengyu

PY - 2015/1/12

Y1 - 2015/1/12

N2 - Flight control system consists of flight controller, sensor, and actuator. Currently, the research focuses on the design and optimization of flight controller, regardless the influence of actuator. This paper is devoted to find out the way actuator effects the flight control system in both dynamic and energy consumption by substituting actuator (hydraulic actuator and electro-hydrostatic actuator) model into the model of flight control system. Results revealed that the model with electro-hydrostatic actuator is better than another in energy consumption characteristics, but worse in dynamic characteristics.

AB - Flight control system consists of flight controller, sensor, and actuator. Currently, the research focuses on the design and optimization of flight controller, regardless the influence of actuator. This paper is devoted to find out the way actuator effects the flight control system in both dynamic and energy consumption by substituting actuator (hydraulic actuator and electro-hydrostatic actuator) model into the model of flight control system. Results revealed that the model with electro-hydrostatic actuator is better than another in energy consumption characteristics, but worse in dynamic characteristics.

UR - https://www.scopus.com/pages/publications/84922569147

U2 - 10.1109/CGNCC.2014.7007581

DO - 10.1109/CGNCC.2014.7007581

M3 - 会议稿件

AN - SCOPUS:84922569147

T3 - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

SP - 2618

EP - 2623

BT - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

Y2 - 8 August 2014 through 10 August 2014

ER -

Hu X, Mao Z, Jiao Z , Wu S, Yu X, Li F. Analysis of the characteristics by modeling and simulation of actuator in flight control system. In 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc. 2015. p. 2618-2623. 7007581. (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014). doi: 10.1109/CGNCC.2014.7007581

Analysis of the characteristics by modeling and simulation of actuator in flight control system

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