Dynamics, stability and control characteristics of unmanned compound autogyro

Qing Lin; Zhihao Cai; Yingxun Wang

doi:10.1109/CGNCC.2016.7828880

Dynamics, stability and control characteristics of unmanned compound autogyro

Institute of Unmanned System

Beihang University

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

3 Scopus citations

Abstract

A compound autogyro unmanned aerial vehicle (UAV) augmented with tip-jet technology is proposed. A nonlinear six/seven-degree-of-freedom model is built, in which the rotor model is control-oriented and bulit based on explicit blade element method. The model is trimmed with fly-to-trim method and a novel multi-mode trim strategy. Based on the trim results, the nonlinear model is linearization and then the dynamic modes, stability and control characteristics throughout the speed range are analyzed. The trim and analyzed results reflect some key features of multi-mode flight and provide good references for autopilot design of the compound autogyro UAV.

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	753-758
Number of pages	6
ISBN (Electronic)	9781467383189
DOIs	https://doi.org/10.1109/CGNCC.2016.7828880
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

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10.1109/CGNCC.2016.7828880

Cite this

Lin, Q., Cai, Z., & Wang, Y. (2017). Dynamics, stability and control characteristics of unmanned compound autogyro. In CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference (pp. 753-758). Article 7828880 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2016.7828880

@inproceedings{11511e81b2d347a8bc0c890296313fd6,

title = "Dynamics, stability and control characteristics of unmanned compound autogyro",

abstract = "A compound autogyro unmanned aerial vehicle (UAV) augmented with tip-jet technology is proposed. A nonlinear six/seven-degree-of-freedom model is built, in which the rotor model is control-oriented and bulit based on explicit blade element method. The model is trimmed with fly-to-trim method and a novel multi-mode trim strategy. Based on the trim results, the nonlinear model is linearization and then the dynamic modes, stability and control characteristics throughout the speed range are analyzed. The trim and analyzed results reflect some key features of multi-mode flight and provide good references for autopilot design of the compound autogyro UAV.",

author = "Qing Lin and Zhihao Cai and Yingxun Wang",

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.2016.7828880",

language = "英语",

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

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

pages = "753--758",

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

address = "美国",

}

Lin, Q, Cai, Z & Wang, Y 2017, Dynamics, stability and control characteristics of unmanned compound autogyro. in CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference., 7828880, CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference, Institute of Electrical and Electronics Engineers Inc., pp. 753-758, 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016, Nanjing, Jiangsu, China, 12/08/16. https://doi.org/10.1109/CGNCC.2016.7828880

Dynamics, stability and control characteristics of unmanned compound autogyro. / Lin, Qing; Cai, Zhihao ; Wang, Yingxun.
CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc., 2017. p. 753-758 7828880 (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 - Dynamics, stability and control characteristics of unmanned compound autogyro

AU - Lin, Qing

AU - Cai, Zhihao

AU - Wang, Yingxun

PY - 2017/1/20

Y1 - 2017/1/20

N2 - A compound autogyro unmanned aerial vehicle (UAV) augmented with tip-jet technology is proposed. A nonlinear six/seven-degree-of-freedom model is built, in which the rotor model is control-oriented and bulit based on explicit blade element method. The model is trimmed with fly-to-trim method and a novel multi-mode trim strategy. Based on the trim results, the nonlinear model is linearization and then the dynamic modes, stability and control characteristics throughout the speed range are analyzed. The trim and analyzed results reflect some key features of multi-mode flight and provide good references for autopilot design of the compound autogyro UAV.

AB - A compound autogyro unmanned aerial vehicle (UAV) augmented with tip-jet technology is proposed. A nonlinear six/seven-degree-of-freedom model is built, in which the rotor model is control-oriented and bulit based on explicit blade element method. The model is trimmed with fly-to-trim method and a novel multi-mode trim strategy. Based on the trim results, the nonlinear model is linearization and then the dynamic modes, stability and control characteristics throughout the speed range are analyzed. The trim and analyzed results reflect some key features of multi-mode flight and provide good references for autopilot design of the compound autogyro UAV.

UR - https://www.scopus.com/pages/publications/85015160777

U2 - 10.1109/CGNCC.2016.7828880

DO - 10.1109/CGNCC.2016.7828880

M3 - 会议稿件

AN - SCOPUS:85015160777

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

SP - 753

EP - 758

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 -

Lin Q, Cai Z , Wang Y. Dynamics, stability and control characteristics of unmanned compound autogyro. In CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc. 2017. p. 753-758. 7828880. (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference). doi: 10.1109/CGNCC.2016.7828880

Dynamics, stability and control characteristics of unmanned compound autogyro

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