Modeling and Robust Attitude Controller Design of a Distributed Propulsion Tilt-Wing UAV in Hovering Flight

Siqi Wang; Bifeng Song; Lei He; Xinyu Lang

doi:10.1109/CCDC.2019.8832344

Modeling and Robust Attitude Controller Design of a Distributed Propulsion Tilt-Wing UAV in Hovering Flight

Siqi Wang, Bifeng Song, Lei He, Xinyu Lang

航空学院

Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

3 引用（Scopus）

摘要

This paper is determined to establish the dynamic model for a distributed propulsion tilt-wing UAV and design a robust attitude controller. Firstly, a detailed dynamic model including the aerodynamic model of propulsion and slipstream towards the target UAV is established. Secondly, an optimal control allocation model that concerns eight kinds of control surfaces is described. Thirdly, based on the established model, a MIMO robust attitude controller containing a 3-dimension LQG controller and a MIMO H-infinity based disturbance observer is determined. Finally, a simulation is designed to verify the whole controller, whose results reach the request.

源语言	英语
主期刊名	Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019
出版商	Institute of Electrical and Electronics Engineers Inc.
页	1480-1485
页数	6
ISBN（电子版）	9781728101057
DOI	https://doi.org/10.1109/CCDC.2019.8832344
出版状态	已出版 - 6月 2019
活动	31st Chinese Control and Decision Conference, CCDC 2019 - Nanchang, 中国期限: 3 6月 2019 → 5 6月 2019

出版系列

姓名	Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019

会议

会议	31st Chinese Control and Decision Conference, CCDC 2019
国家/地区	中国
市	Nanchang
时期	3/06/19 → 5/06/19

访问文件

10.1109/CCDC.2019.8832344

其它文件与链接

链接到 Scopus 的出版物

引用此

Wang, S., Song, B., He, L., & Lang, X. (2019). Modeling and Robust Attitude Controller Design of a Distributed Propulsion Tilt-Wing UAV in Hovering Flight. 在 Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019 (页码 1480-1485). 文章 8832344 (Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC.2019.8832344

Wang, Siqi ; Song, Bifeng ; He, Lei 等. / Modeling and Robust Attitude Controller Design of a Distributed Propulsion Tilt-Wing UAV in Hovering Flight. Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019. Institute of Electrical and Electronics Engineers Inc., 2019. 页码 1480-1485 (Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019).

@inproceedings{76cc9d0762e343b1befb25bb213dfdd5,

title = "Modeling and Robust Attitude Controller Design of a Distributed Propulsion Tilt-Wing UAV in Hovering Flight",

abstract = "This paper is determined to establish the dynamic model for a distributed propulsion tilt-wing UAV and design a robust attitude controller. Firstly, a detailed dynamic model including the aerodynamic model of propulsion and slipstream towards the target UAV is established. Secondly, an optimal control allocation model that concerns eight kinds of control surfaces is described. Thirdly, based on the established model, a MIMO robust attitude controller containing a 3-dimension LQG controller and a MIMO H-infinity based disturbance observer is determined. Finally, a simulation is designed to verify the whole controller, whose results reach the request.",

keywords = "DOB, Optimal Control Allocation, Robust Attitude Controller, Tilt-Wing UAV",

author = "Siqi Wang and Bifeng Song and Lei He and Xinyu Lang",

note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 31st Chinese Control and Decision Conference, CCDC 2019 ; Conference date: 03-06-2019 Through 05-06-2019",

year = "2019",

month = jun,

doi = "10.1109/CCDC.2019.8832344",

language = "英语",

series = "Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019",

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

pages = "1480--1485",

booktitle = "Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019",

}

Wang, S, Song, B, He, L & Lang, X 2019, Modeling and Robust Attitude Controller Design of a Distributed Propulsion Tilt-Wing UAV in Hovering Flight. 在 Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019., 8832344, Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019, Institute of Electrical and Electronics Engineers Inc., 页码 1480-1485, 31st Chinese Control and Decision Conference, CCDC 2019, Nanchang, 中国, 3/06/19. https://doi.org/10.1109/CCDC.2019.8832344

Modeling and Robust Attitude Controller Design of a Distributed Propulsion Tilt-Wing UAV in Hovering Flight. / Wang, Siqi; Song, Bifeng; He, Lei 等.
Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019. Institute of Electrical and Electronics Engineers Inc., 2019. 页码 1480-1485 8832344 (Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Modeling and Robust Attitude Controller Design of a Distributed Propulsion Tilt-Wing UAV in Hovering Flight

AU - Wang, Siqi

AU - Song, Bifeng

AU - He, Lei

AU - Lang, Xinyu

PY - 2019/6

Y1 - 2019/6

N2 - This paper is determined to establish the dynamic model for a distributed propulsion tilt-wing UAV and design a robust attitude controller. Firstly, a detailed dynamic model including the aerodynamic model of propulsion and slipstream towards the target UAV is established. Secondly, an optimal control allocation model that concerns eight kinds of control surfaces is described. Thirdly, based on the established model, a MIMO robust attitude controller containing a 3-dimension LQG controller and a MIMO H-infinity based disturbance observer is determined. Finally, a simulation is designed to verify the whole controller, whose results reach the request.

AB - This paper is determined to establish the dynamic model for a distributed propulsion tilt-wing UAV and design a robust attitude controller. Firstly, a detailed dynamic model including the aerodynamic model of propulsion and slipstream towards the target UAV is established. Secondly, an optimal control allocation model that concerns eight kinds of control surfaces is described. Thirdly, based on the established model, a MIMO robust attitude controller containing a 3-dimension LQG controller and a MIMO H-infinity based disturbance observer is determined. Finally, a simulation is designed to verify the whole controller, whose results reach the request.

KW - DOB

KW - Optimal Control Allocation

KW - Robust Attitude Controller

KW - Tilt-Wing UAV

UR - http://www.scopus.com/inward/record.url?scp=85073116511&partnerID=8YFLogxK

U2 - 10.1109/CCDC.2019.8832344

DO - 10.1109/CCDC.2019.8832344

M3 - 会议稿件

AN - SCOPUS:85073116511

T3 - Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019

SP - 1480

EP - 1485

BT - Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 31st Chinese Control and Decision Conference, CCDC 2019

Y2 - 3 June 2019 through 5 June 2019

ER -

Wang S, Song B, He L, Lang X. Modeling and Robust Attitude Controller Design of a Distributed Propulsion Tilt-Wing UAV in Hovering Flight. 在 Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019. Institute of Electrical and Electronics Engineers Inc. 2019. 页码 1480-1485. 8832344. (Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019). doi: 10.1109/CCDC.2019.8832344

Modeling and Robust Attitude Controller Design of a Distributed Propulsion Tilt-Wing UAV in Hovering Flight

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