Research on the attitude control of unmanned multi-ducted-fan flying vehicle

Yue Ma; Wanming Chen; Lu Lin; Yu Wang

doi:10.1109/ICSTCC.2017.8107054

Research on the attitude control of unmanned multi-ducted-fan flying vehicle

Yue Ma, Wanming Chen, Lu Lin, Yu Wang

School of Mechanical Engineering

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

Abstract

The unmanned multi-ducted-fan flying vehicle is a kind of novel multi-purpose platform for future transportation. In this paper, flight dynamics model is established based on aerodynamics principles and rigid body dynamics theory. To make the controller of the multi-ducted fan flying vehicle more robust, a double closed loop PID controller is put forward with non-smooth parameters optimization method. Numerical simulation and field the experimental results demonstrate that the PID controller has good performance on the inner-loop attitude control in forward flight.

Original language	English
Title of host publication	2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017
Editors	Marius Kloetzer, Lavinia Ferariu
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	321-327
Number of pages	7
ISBN (Electronic)	9781538638422
DOIs	https://doi.org/10.1109/ICSTCC.2017.8107054
Publication status	Published - 13 Nov 2017
Event	21st International Conference on System Theory, Control and Computing, ICSTCC 2017 - Sinaia, Romania Duration: 19 Oct 2017 → 21 Oct 2017

Publication series

Name	2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017

Conference

Conference	21st International Conference on System Theory, Control and Computing, ICSTCC 2017
Country/Territory	Romania
City	Sinaia
Period	19/10/17 → 21/10/17

Keywords

double closed loop PID
multi-ducted-fan flying vehicle
non-smooth optimization

Access to Document

10.1109/ICSTCC.2017.8107054

Cite this

Ma, Y., Chen, W., Lin, L., & Wang, Y. (2017). Research on the attitude control of unmanned multi-ducted-fan flying vehicle. In M. Kloetzer, & L. Ferariu (Eds.), 2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017 (pp. 321-327). Article 8107054 (2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICSTCC.2017.8107054

Ma, Yue ; Chen, Wanming ; Lin, Lu et al. / Research on the attitude control of unmanned multi-ducted-fan flying vehicle. 2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017. editor / Marius Kloetzer ; Lavinia Ferariu. Institute of Electrical and Electronics Engineers Inc., 2017. pp. 321-327 (2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017).

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title = "Research on the attitude control of unmanned multi-ducted-fan flying vehicle",

abstract = "The unmanned multi-ducted-fan flying vehicle is a kind of novel multi-purpose platform for future transportation. In this paper, flight dynamics model is established based on aerodynamics principles and rigid body dynamics theory. To make the controller of the multi-ducted fan flying vehicle more robust, a double closed loop PID controller is put forward with non-smooth parameters optimization method. Numerical simulation and field the experimental results demonstrate that the PID controller has good performance on the inner-loop attitude control in forward flight.",

keywords = "double closed loop PID, multi-ducted-fan flying vehicle, non-smooth optimization",

author = "Yue Ma and Wanming Chen and Lu Lin and Yu Wang",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 21st International Conference on System Theory, Control and Computing, ICSTCC 2017 ; Conference date: 19-10-2017 Through 21-10-2017",

year = "2017",

month = nov,

day = "13",

doi = "10.1109/ICSTCC.2017.8107054",

language = "English",

series = "2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017",

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

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editor = "Marius Kloetzer and Lavinia Ferariu",

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Ma, Y, Chen, W, Lin, L & Wang, Y 2017, Research on the attitude control of unmanned multi-ducted-fan flying vehicle. in M Kloetzer & L Ferariu (eds), 2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017., 8107054, 2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017, Institute of Electrical and Electronics Engineers Inc., pp. 321-327, 21st International Conference on System Theory, Control and Computing, ICSTCC 2017, Sinaia, Romania, 19/10/17. https://doi.org/10.1109/ICSTCC.2017.8107054

Research on the attitude control of unmanned multi-ducted-fan flying vehicle. / Ma, Yue; Chen, Wanming; Lin, Lu et al.
2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017. ed. / Marius Kloetzer; Lavinia Ferariu. Institute of Electrical and Electronics Engineers Inc., 2017. p. 321-327 8107054 (2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017).

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

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N2 - The unmanned multi-ducted-fan flying vehicle is a kind of novel multi-purpose platform for future transportation. In this paper, flight dynamics model is established based on aerodynamics principles and rigid body dynamics theory. To make the controller of the multi-ducted fan flying vehicle more robust, a double closed loop PID controller is put forward with non-smooth parameters optimization method. Numerical simulation and field the experimental results demonstrate that the PID controller has good performance on the inner-loop attitude control in forward flight.

AB - The unmanned multi-ducted-fan flying vehicle is a kind of novel multi-purpose platform for future transportation. In this paper, flight dynamics model is established based on aerodynamics principles and rigid body dynamics theory. To make the controller of the multi-ducted fan flying vehicle more robust, a double closed loop PID controller is put forward with non-smooth parameters optimization method. Numerical simulation and field the experimental results demonstrate that the PID controller has good performance on the inner-loop attitude control in forward flight.

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Ma Y, Chen W, Lin L, Wang Y. Research on the attitude control of unmanned multi-ducted-fan flying vehicle. In Kloetzer M, Ferariu L, editors, 2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017. Institute of Electrical and Electronics Engineers Inc. 2017. p. 321-327. 8107054. (2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017). doi: 10.1109/ICSTCC.2017.8107054

Research on the attitude control of unmanned multi-ducted-fan flying vehicle

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Keywords

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