Ducted fan UAV hovering attitude control

Xiao Lu Ren; Chang Hong Wang; Guo Xing Yi

doi:10.1109/EMEIT.2011.6022908

Ducted fan UAV hovering attitude control

Xiao Lu Ren^*
, Chang Hong Wang
, Guo Xing Yi

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

5 Scopus citations

Abstract

This paper focus on the modeling and control of a small ducted fan unmanned aerial vehicle (UAV). The mathematical model of the hovering flight UAV is established from aerodynamic analysis. Then, a control method for the hovering flight was obtained, which is based on the H_∞ control theory. By this method, the closed-loop poles of the system were placed at a prescribed disk region. The simulation results show that this method can provide the robust stability as well as the good dynamic performance and anti-disturbance capacity.

Original language	English
Title of host publication	Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
Pages	421-424
Number of pages	4
DOIs	https://doi.org/10.1109/EMEIT.2011.6022908
State	Published - 2011
Event	2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011 - Harbin, China Duration: 12 Aug 2011 → 14 Aug 2011

Publication series

Name	Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
Volume	1

Conference

Conference	2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
Country/Territory	China
City	Harbin
Period	12/08/11 → 14/08/11

Keywords

H Control
Regional Pole Constraints
State Feedback
Unmaned Aerial Vehicles(UAV)

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10.1109/EMEIT.2011.6022908

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Ren, X. L., Wang, C. H., & Yi, G. X. (2011). Ducted fan UAV hovering attitude control. In Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011 (pp. 421-424). Article 6022908 (Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011; Vol. 1). https://doi.org/10.1109/EMEIT.2011.6022908

@inproceedings{9c3937e264304f5789bf64e1ee5201c3,

title = "Ducted fan UAV hovering attitude control",

abstract = "This paper focus on the modeling and control of a small ducted fan unmanned aerial vehicle (UAV). The mathematical model of the hovering flight UAV is established from aerodynamic analysis. Then, a control method for the hovering flight was obtained, which is based on the H∞ control theory. By this method, the closed-loop poles of the system were placed at a prescribed disk region. The simulation results show that this method can provide the robust stability as well as the good dynamic performance and anti-disturbance capacity.",

keywords = "H Control, Regional Pole Constraints, State Feedback, Unmaned Aerial Vehicles(UAV)",

author = "Ren, \{Xiao Lu\} and Wang, \{Chang Hong\} and Yi, \{Guo Xing\}",

year = "2011",

doi = "10.1109/EMEIT.2011.6022908",

language = "英语",

isbn = "9781612840857",

series = "Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011",

pages = "421--424",

booktitle = "Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011",

note = "2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011 ; Conference date: 12-08-2011 Through 14-08-2011",

}

Ren, XL, Wang, CH & Yi, GX 2011, Ducted fan UAV hovering attitude control. in Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011., 6022908, Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011, vol. 1, pp. 421-424, 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011, Harbin, China, 12/08/11. https://doi.org/10.1109/EMEIT.2011.6022908

Ducted fan UAV hovering attitude control. / Ren, Xiao Lu; Wang, Chang Hong ; Yi, Guo Xing.
Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011. 2011. p. 421-424 6022908 (Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011; Vol. 1).

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

TY - GEN

T1 - Ducted fan UAV hovering attitude control

AU - Ren, Xiao Lu

AU - Wang, Chang Hong

AU - Yi, Guo Xing

PY - 2011

Y1 - 2011

N2 - This paper focus on the modeling and control of a small ducted fan unmanned aerial vehicle (UAV). The mathematical model of the hovering flight UAV is established from aerodynamic analysis. Then, a control method for the hovering flight was obtained, which is based on the H∞ control theory. By this method, the closed-loop poles of the system were placed at a prescribed disk region. The simulation results show that this method can provide the robust stability as well as the good dynamic performance and anti-disturbance capacity.

AB - This paper focus on the modeling and control of a small ducted fan unmanned aerial vehicle (UAV). The mathematical model of the hovering flight UAV is established from aerodynamic analysis. Then, a control method for the hovering flight was obtained, which is based on the H∞ control theory. By this method, the closed-loop poles of the system were placed at a prescribed disk region. The simulation results show that this method can provide the robust stability as well as the good dynamic performance and anti-disturbance capacity.

KW - H Control

KW - Regional Pole Constraints

KW - State Feedback

KW - Unmaned Aerial Vehicles(UAV)

UR - https://www.scopus.com/pages/publications/80053408230

U2 - 10.1109/EMEIT.2011.6022908

DO - 10.1109/EMEIT.2011.6022908

M3 - 会议稿件

AN - SCOPUS:80053408230

SN - 9781612840857

T3 - Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011

SP - 421

EP - 424

BT - Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011

T2 - 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011

Y2 - 12 August 2011 through 14 August 2011

ER -

Ren XL, Wang CH , Yi GX. Ducted fan UAV hovering attitude control. In Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011. 2011. p. 421-424. 6022908. (Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011). doi: 10.1109/EMEIT.2011.6022908

Ducted fan UAV hovering attitude control

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