Model and Attitude Control of a Miniature Hybrid Autogyro

Ziwei Song; Zhihao Cai; Kunpeng Li; Jiang Zhao; Ningjun Liu

doi:10.1007/978-981-10-6445-6_82

Model and Attitude Control of a Miniature Hybrid Autogyro

Ziwei Song^*
, Zhihao Cai
, Kunpeng Li
, Jiang Zhao
, Ningjun Liu

^*Corresponding author for this work

Beihang University

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

3 Scopus citations

Abstract

In this paper, we focus on the hybrid autogyro, which is a combination of autogyro and fixed-wing aircraft. To explore the flight characteristics and improve the control quality, a dynamics model is established, in which the rotor dynamics are modeled via an explicit mathematical form of blade element theory. Due to the complex structure of the hybrid layout UAV, the aerodynamic interference between the parts is strong, and the model has strong nonlinearity and certain uncertainty. We choose back-stepping control method to design the attitude controller. The result shows that the controller can successfully control the hybrid autogyro’s roll, pitch and yaw angles. Tracking is quick and largely satisfactory, with good stability.

Original language	English
Title of host publication	Proceedings of 2017 Chinese Intelligent Automation Conference
Editors	Zhidong Deng
Publisher	Springer Verlag
Pages	751-760
Number of pages	10
ISBN (Print)	9789811064449
DOIs	https://doi.org/10.1007/978-981-10-6445-6_82
State	Published - 2018
Event	Chinese Intelligent Automation Conference, CIAC 2017 - Tianjin, China Duration: 2 Jun 2017 → 4 Jun 2017

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	458
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	Chinese Intelligent Automation Conference, CIAC 2017
Country/Territory	China
City	Tianjin
Period	2/06/17 → 4/06/17

Keywords

Attitude control
Back-stepping method
Dynamics modelling
Hybrid autogyro

Access to Document

10.1007/978-981-10-6445-6_82

Cite this

@inproceedings{a2a021a546f64be8b76eedd643f4a0ee,

title = "Model and Attitude Control of a Miniature Hybrid Autogyro",

abstract = "In this paper, we focus on the hybrid autogyro, which is a combination of autogyro and fixed-wing aircraft. To explore the flight characteristics and improve the control quality, a dynamics model is established, in which the rotor dynamics are modeled via an explicit mathematical form of blade element theory. Due to the complex structure of the hybrid layout UAV, the aerodynamic interference between the parts is strong, and the model has strong nonlinearity and certain uncertainty. We choose back-stepping control method to design the attitude controller. The result shows that the controller can successfully control the hybrid autogyro{\textquoteright}s roll, pitch and yaw angles. Tracking is quick and largely satisfactory, with good stability.",

keywords = "Attitude control, Back-stepping method, Dynamics modelling, Hybrid autogyro",

author = "Ziwei Song and Zhihao Cai and Kunpeng Li and Jiang Zhao and Ningjun Liu",

note = "Publisher Copyright: {\textcopyright} 2018, Springer Nature Singapore Pte Ltd.; Chinese Intelligent Automation Conference, CIAC 2017 ; Conference date: 02-06-2017 Through 04-06-2017",

year = "2018",

doi = "10.1007/978-981-10-6445-6\_82",

language = "英语",

isbn = "9789811064449",

series = "Lecture Notes in Electrical Engineering",

publisher = "Springer Verlag",

pages = "751--760",

editor = "Zhidong Deng",

booktitle = "Proceedings of 2017 Chinese Intelligent Automation Conference",

address = "德国",

}

Song, Z, Cai, Z, Li, K, Zhao, J & Liu, N 2018, Model and Attitude Control of a Miniature Hybrid Autogyro. in Z Deng (ed.), Proceedings of 2017 Chinese Intelligent Automation Conference. Lecture Notes in Electrical Engineering, vol. 458, Springer Verlag, pp. 751-760, Chinese Intelligent Automation Conference, CIAC 2017, Tianjin, China, 2/06/17. https://doi.org/10.1007/978-981-10-6445-6_82

Model and Attitude Control of a Miniature Hybrid Autogyro. / Song, Ziwei; Cai, Zhihao; Li, Kunpeng et al.
Proceedings of 2017 Chinese Intelligent Automation Conference. ed. / Zhidong Deng. Springer Verlag, 2018. p. 751-760 (Lecture Notes in Electrical Engineering; Vol. 458).

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

TY - GEN

T1 - Model and Attitude Control of a Miniature Hybrid Autogyro

AU - Song, Ziwei

AU - Cai, Zhihao

AU - Li, Kunpeng

AU - Zhao, Jiang

AU - Liu, Ningjun

PY - 2018

Y1 - 2018

N2 - In this paper, we focus on the hybrid autogyro, which is a combination of autogyro and fixed-wing aircraft. To explore the flight characteristics and improve the control quality, a dynamics model is established, in which the rotor dynamics are modeled via an explicit mathematical form of blade element theory. Due to the complex structure of the hybrid layout UAV, the aerodynamic interference between the parts is strong, and the model has strong nonlinearity and certain uncertainty. We choose back-stepping control method to design the attitude controller. The result shows that the controller can successfully control the hybrid autogyro’s roll, pitch and yaw angles. Tracking is quick and largely satisfactory, with good stability.

AB - In this paper, we focus on the hybrid autogyro, which is a combination of autogyro and fixed-wing aircraft. To explore the flight characteristics and improve the control quality, a dynamics model is established, in which the rotor dynamics are modeled via an explicit mathematical form of blade element theory. Due to the complex structure of the hybrid layout UAV, the aerodynamic interference between the parts is strong, and the model has strong nonlinearity and certain uncertainty. We choose back-stepping control method to design the attitude controller. The result shows that the controller can successfully control the hybrid autogyro’s roll, pitch and yaw angles. Tracking is quick and largely satisfactory, with good stability.

KW - Attitude control

KW - Back-stepping method

KW - Dynamics modelling

KW - Hybrid autogyro

UR - https://www.scopus.com/pages/publications/85034034817

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DO - 10.1007/978-981-10-6445-6_82

M3 - 会议稿件

AN - SCOPUS:85034034817

SN - 9789811064449

T3 - Lecture Notes in Electrical Engineering

SP - 751

EP - 760

BT - Proceedings of 2017 Chinese Intelligent Automation Conference

A2 - Deng, Zhidong

PB - Springer Verlag

T2 - Chinese Intelligent Automation Conference, CIAC 2017

Y2 - 2 June 2017 through 4 June 2017

ER -

Model and Attitude Control of a Miniature Hybrid Autogyro

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Keywords

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