Modeling and control for morphing unmanned aircraft vehicle

Mengtao Li; Lei Guo; Kejian Wu

doi:10.1109/CGNCC.2016.7828963

Modeling and control for morphing unmanned aircraft vehicle

Mengtao Li
, Lei Guo^*
, Kejian Wu

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University

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

5 Scopus citations

Abstract

there has been wide interest in the research of Mars exploration. Morphing unmanned aircraft vehicle (MUAV) is one of most promising vehicles to execute special tasks in Mars exploration missions for its better aerodynamic characteristics compared with the conventional fixed wing vehicle. Modeling and control for MUAV are difficult problems. In this paper, firstly, the nonlinear six-degree-of-freedom (6DOF) dynamic model for MUAV is established, considering the asymmetry of the rotating wing. Secondly, control system is presented for the morphing aircraft based nonlinear dynamic inversion method. Finally, real-time simulation results are given to illustrate the control scheme can meet the requirements of attitude control.

Original language	English
Title of host publication	CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1226-1231
Number of pages	6
ISBN (Electronic)	9781467383189
DOIs	https://doi.org/10.1109/CGNCC.2016.7828963
State	Published - 20 Jan 2017
Event	7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 - Nanjing, Jiangsu, China Duration: 12 Aug 2016 → 14 Aug 2016

Publication series

Name	CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

Conference

Conference	7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Country/Territory	China
City	Nanjing, Jiangsu
Period	12/08/16 → 14/08/16

Keywords

6DOF
Modeling
Morphing unmanned aircraft vehicle
Nonlinear dynamic inversion method

Access to Document

10.1109/CGNCC.2016.7828963

Cite this

Li, M., Guo, L., & Wu, K. (2017). Modeling and control for morphing unmanned aircraft vehicle. In CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference (pp. 1226-1231). Article 7828963 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2016.7828963

@inproceedings{87d4d601f1494f0b988d00a50f5bd347,

title = "Modeling and control for morphing unmanned aircraft vehicle",

abstract = "there has been wide interest in the research of Mars exploration. Morphing unmanned aircraft vehicle (MUAV) is one of most promising vehicles to execute special tasks in Mars exploration missions for its better aerodynamic characteristics compared with the conventional fixed wing vehicle. Modeling and control for MUAV are difficult problems. In this paper, firstly, the nonlinear six-degree-of-freedom (6DOF) dynamic model for MUAV is established, considering the asymmetry of the rotating wing. Secondly, control system is presented for the morphing aircraft based nonlinear dynamic inversion method. Finally, real-time simulation results are given to illustrate the control scheme can meet the requirements of attitude control.",

keywords = "6DOF, Modeling, Morphing unmanned aircraft vehicle, Nonlinear dynamic inversion method",

author = "Mengtao Li and Lei Guo and Kejian Wu",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 ; Conference date: 12-08-2016 Through 14-08-2016",

year = "2017",

month = jan,

day = "20",

doi = "10.1109/CGNCC.2016.7828963",

language = "英语",

series = "CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference",

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

pages = "1226--1231",

booktitle = "CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference",

address = "美国",

}

Li, M, Guo, L & Wu, K 2017, Modeling and control for morphing unmanned aircraft vehicle. in CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference., 7828963, CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference, Institute of Electrical and Electronics Engineers Inc., pp. 1226-1231, 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016, Nanjing, Jiangsu, China, 12/08/16. https://doi.org/10.1109/CGNCC.2016.7828963

Modeling and control for morphing unmanned aircraft vehicle. / Li, Mengtao; Guo, Lei; Wu, Kejian.
CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc., 2017. p. 1226-1231 7828963 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference).

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

TY - GEN

T1 - Modeling and control for morphing unmanned aircraft vehicle

AU - Li, Mengtao

AU - Guo, Lei

AU - Wu, Kejian

PY - 2017/1/20

Y1 - 2017/1/20

N2 - there has been wide interest in the research of Mars exploration. Morphing unmanned aircraft vehicle (MUAV) is one of most promising vehicles to execute special tasks in Mars exploration missions for its better aerodynamic characteristics compared with the conventional fixed wing vehicle. Modeling and control for MUAV are difficult problems. In this paper, firstly, the nonlinear six-degree-of-freedom (6DOF) dynamic model for MUAV is established, considering the asymmetry of the rotating wing. Secondly, control system is presented for the morphing aircraft based nonlinear dynamic inversion method. Finally, real-time simulation results are given to illustrate the control scheme can meet the requirements of attitude control.

AB - there has been wide interest in the research of Mars exploration. Morphing unmanned aircraft vehicle (MUAV) is one of most promising vehicles to execute special tasks in Mars exploration missions for its better aerodynamic characteristics compared with the conventional fixed wing vehicle. Modeling and control for MUAV are difficult problems. In this paper, firstly, the nonlinear six-degree-of-freedom (6DOF) dynamic model for MUAV is established, considering the asymmetry of the rotating wing. Secondly, control system is presented for the morphing aircraft based nonlinear dynamic inversion method. Finally, real-time simulation results are given to illustrate the control scheme can meet the requirements of attitude control.

KW - 6DOF

KW - Modeling

KW - Morphing unmanned aircraft vehicle

KW - Nonlinear dynamic inversion method

UR - https://www.scopus.com/pages/publications/85015185634

U2 - 10.1109/CGNCC.2016.7828963

DO - 10.1109/CGNCC.2016.7828963

M3 - 会议稿件

AN - SCOPUS:85015185634

T3 - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

SP - 1226

EP - 1231

BT - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016

Y2 - 12 August 2016 through 14 August 2016

ER -

Modeling and control for morphing unmanned aircraft vehicle

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