Dynamic analysis and CFD calculation of a differential control type for ducted fan UAV

Feng Weiwei; Wu Yanxuan; Chen Yang; Wang Zhengjie

doi:10.1109/ICMIC.2014.7020760

Dynamic analysis and CFD calculation of a differential control type for ducted fan UAV

Feng Weiwei
, Wu Yanxuan
, Chen Yang
, Wang Zhengjie

School of Automation

Beijing Institute of Technology

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

2 Citations (Scopus)

Abstract

In recent years, 'Smart City' has been developing and need to obtain accurately information of the city, As a movable platform for sensing detection system in air, the ducted fan UAV will play an important role for information collecting in the complex urban environment. Because the complexity of traditional ducted fan UAV's control organ, which has strong air coupling, so there has big challenge if this kind of ducted fan UAV is used in the complex urban environment. A differential control type for ducted fan UAV has presented in this paper, through dynamics analysis and CFD simulation to the traditional ducted fan UAV and differential control type, the differential control type can keep the yaw stability of aircraft when the control flaps has a rational angle and stable lift when the control flaps become, meanwhile it can control the pitch and roll attitude through the differential motion of control flaps. So this differential control type is feasible and possesses some advantage over relative to traditional type if processing reasonable optimization and design.

Original language	English
Title of host publication	Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	249-253
Number of pages	5
ISBN (Electronic)	9780956715746
DOIs	https://doi.org/10.1109/ICMIC.2014.7020760
Publication status	Published - 23 Jan 2015
Event	6th International Conference on Modelling, Identification and Control, ICMIC 2014 - Melbourne, Australia Duration: 3 Dec 2014 → 5 Dec 2014

Publication series

Name	Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014

Conference

Conference	6th International Conference on Modelling, Identification and Control, ICMIC 2014
Country/Territory	Australia
City	Melbourne
Period	3/12/14 → 5/12/14

UN SDGs

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

SDG 11 Sustainable Cities and Communities

Keywords

CFD calculation
differential control
ducted fan UAV
dynamic analysis

Access to Document

10.1109/ICMIC.2014.7020760

Cite this

Weiwei, F., Yanxuan, W., Yang, C., & Zhengjie, W. (2015). Dynamic analysis and CFD calculation of a differential control type for ducted fan UAV. In Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014 (pp. 249-253). Article 7020760 (Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICMIC.2014.7020760

Weiwei, Feng ; Yanxuan, Wu ; Yang, Chen et al. / Dynamic analysis and CFD calculation of a differential control type for ducted fan UAV. Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014. Institute of Electrical and Electronics Engineers Inc., 2015. pp. 249-253 (Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014).

@inproceedings{f04c18d92bd04181a8126f0c58e9d944,

title = "Dynamic analysis and CFD calculation of a differential control type for ducted fan UAV",

abstract = "In recent years, 'Smart City' has been developing and need to obtain accurately information of the city, As a movable platform for sensing detection system in air, the ducted fan UAV will play an important role for information collecting in the complex urban environment. Because the complexity of traditional ducted fan UAV's control organ, which has strong air coupling, so there has big challenge if this kind of ducted fan UAV is used in the complex urban environment. A differential control type for ducted fan UAV has presented in this paper, through dynamics analysis and CFD simulation to the traditional ducted fan UAV and differential control type, the differential control type can keep the yaw stability of aircraft when the control flaps has a rational angle and stable lift when the control flaps become, meanwhile it can control the pitch and roll attitude through the differential motion of control flaps. So this differential control type is feasible and possesses some advantage over relative to traditional type if processing reasonable optimization and design.",

keywords = "CFD calculation, differential control, ducted fan UAV, dynamic analysis",

author = "Feng Weiwei and Wu Yanxuan and Chen Yang and Wang Zhengjie",

note = "Publisher Copyright: {\textcopyright} 2014 Swinburne University of Technology, Australia.; 6th International Conference on Modelling, Identification and Control, ICMIC 2014 ; Conference date: 03-12-2014 Through 05-12-2014",

year = "2015",

month = jan,

day = "23",

doi = "10.1109/ICMIC.2014.7020760",

language = "English",

series = "Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014",

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

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booktitle = "Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014",

address = "United States",

}

Weiwei, F, Yanxuan, W, Yang, C & Zhengjie, W 2015, Dynamic analysis and CFD calculation of a differential control type for ducted fan UAV. in Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014., 7020760, Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014, Institute of Electrical and Electronics Engineers Inc., pp. 249-253, 6th International Conference on Modelling, Identification and Control, ICMIC 2014, Melbourne, Australia, 3/12/14. https://doi.org/10.1109/ICMIC.2014.7020760

Dynamic analysis and CFD calculation of a differential control type for ducted fan UAV. / Weiwei, Feng; Yanxuan, Wu; Yang, Chen et al.
Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014. Institute of Electrical and Electronics Engineers Inc., 2015. p. 249-253 7020760 (Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014).

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

TY - GEN

T1 - Dynamic analysis and CFD calculation of a differential control type for ducted fan UAV

AU - Weiwei, Feng

AU - Yanxuan, Wu

AU - Yang, Chen

AU - Zhengjie, Wang

PY - 2015/1/23

Y1 - 2015/1/23

N2 - In recent years, 'Smart City' has been developing and need to obtain accurately information of the city, As a movable platform for sensing detection system in air, the ducted fan UAV will play an important role for information collecting in the complex urban environment. Because the complexity of traditional ducted fan UAV's control organ, which has strong air coupling, so there has big challenge if this kind of ducted fan UAV is used in the complex urban environment. A differential control type for ducted fan UAV has presented in this paper, through dynamics analysis and CFD simulation to the traditional ducted fan UAV and differential control type, the differential control type can keep the yaw stability of aircraft when the control flaps has a rational angle and stable lift when the control flaps become, meanwhile it can control the pitch and roll attitude through the differential motion of control flaps. So this differential control type is feasible and possesses some advantage over relative to traditional type if processing reasonable optimization and design.

AB - In recent years, 'Smart City' has been developing and need to obtain accurately information of the city, As a movable platform for sensing detection system in air, the ducted fan UAV will play an important role for information collecting in the complex urban environment. Because the complexity of traditional ducted fan UAV's control organ, which has strong air coupling, so there has big challenge if this kind of ducted fan UAV is used in the complex urban environment. A differential control type for ducted fan UAV has presented in this paper, through dynamics analysis and CFD simulation to the traditional ducted fan UAV and differential control type, the differential control type can keep the yaw stability of aircraft when the control flaps has a rational angle and stable lift when the control flaps become, meanwhile it can control the pitch and roll attitude through the differential motion of control flaps. So this differential control type is feasible and possesses some advantage over relative to traditional type if processing reasonable optimization and design.

KW - CFD calculation

KW - differential control

KW - ducted fan UAV

KW - dynamic analysis

UR - https://www.scopus.com/pages/publications/84923474852

U2 - 10.1109/ICMIC.2014.7020760

DO - 10.1109/ICMIC.2014.7020760

M3 - Conference contribution

AN - SCOPUS:84923474852

T3 - Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014

SP - 249

EP - 253

BT - Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 6th International Conference on Modelling, Identification and Control, ICMIC 2014

Y2 - 3 December 2014 through 5 December 2014

ER -

Weiwei F, Yanxuan W, Yang C, Zhengjie W. Dynamic analysis and CFD calculation of a differential control type for ducted fan UAV. In Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014. Institute of Electrical and Electronics Engineers Inc. 2015. p. 249-253. 7020760. (Proceedings of 2014 International Conference on Modelling, Identification and Control, ICMIC 2014). doi: 10.1109/ICMIC.2014.7020760

Dynamic analysis and CFD calculation of a differential control type for ducted fan UAV

Abstract

Publication series

Conference

UN SDGs

Keywords

Access to Document

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