Folding mechanism design and analysis of high-altitude gliding UUV wings

Yilin Li; Baowei Song

doi:10.1109/IAEAC.2017.8054354

Folding mechanism design and analysis of high-altitude gliding UUV wings

Yilin Li, Baowei Song

School of Marine Science and Technology

Northwestern Polytechnical University Xian

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

Abstract

High-altitude gliding unmanned underwater vehicles (HAGUUVs) are released in high attitude and works in water after a short glide in the air. According to the High-altitude Gliding UUV airborne emission requirements, the folding mechanism of wings of the HAGUUV is desighed. On the basis of mechanics analysis of the organization, the dynamics modeling of organization's unfolding process is given by using Lagrange equation, and the wings unfolding movement characteristics are discussed through numerical simulation. Analysis results show that the designed folding mechanism can achieve the requirement of High-altitude gliding system performance, and provides theoretical guidance for further drop experiment.

Original language	English
Title of host publication	Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017
Editors	Bing Xu
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1948-1951
Number of pages	4
ISBN (Electronic)	9781467389778
DOIs	https://doi.org/10.1109/IAEAC.2017.8054354
State	Published - 29 Sep 2017
Event	2nd IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017 - Chongqing, China Duration: 25 Mar 2017 → 26 Mar 2017

Publication series

Name	Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017

Conference

Conference	2nd IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017
Country/Territory	China
City	Chongqing
Period	25/03/17 → 26/03/17

Keywords

Dynamics modeling
Folding wing
High-altitude gliding
Numerical simulation

Access to Document

10.1109/IAEAC.2017.8054354

Cite this

Li, Y., & Song, B. (2017). Folding mechanism design and analysis of high-altitude gliding UUV wings. In B. Xu (Ed.), Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017 (pp. 1948-1951). Article 8054354 (Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/IAEAC.2017.8054354

Li, Yilin ; Song, Baowei. / Folding mechanism design and analysis of high-altitude gliding UUV wings. Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017. editor / Bing Xu. Institute of Electrical and Electronics Engineers Inc., 2017. pp. 1948-1951 (Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017).

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title = "Folding mechanism design and analysis of high-altitude gliding UUV wings",

abstract = "High-altitude gliding unmanned underwater vehicles (HAGUUVs) are released in high attitude and works in water after a short glide in the air. According to the High-altitude Gliding UUV airborne emission requirements, the folding mechanism of wings of the HAGUUV is desighed. On the basis of mechanics analysis of the organization, the dynamics modeling of organization's unfolding process is given by using Lagrange equation, and the wings unfolding movement characteristics are discussed through numerical simulation. Analysis results show that the designed folding mechanism can achieve the requirement of High-altitude gliding system performance, and provides theoretical guidance for further drop experiment.",

keywords = "Dynamics modeling, Folding wing, High-altitude gliding, Numerical simulation",

author = "Yilin Li and Baowei Song",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 2nd IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017 ; Conference date: 25-03-2017 Through 26-03-2017",

year = "2017",

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doi = "10.1109/IAEAC.2017.8054354",

language = "英语",

series = "Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017",

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

pages = "1948--1951",

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booktitle = "Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017",

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Li, Y & Song, B 2017, Folding mechanism design and analysis of high-altitude gliding UUV wings. in B Xu (ed.), Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017., 8054354, Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017, Institute of Electrical and Electronics Engineers Inc., pp. 1948-1951, 2nd IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017, Chongqing, China, 25/03/17. https://doi.org/10.1109/IAEAC.2017.8054354

Folding mechanism design and analysis of high-altitude gliding UUV wings. / Li, Yilin; Song, Baowei.
Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017. ed. / Bing Xu. Institute of Electrical and Electronics Engineers Inc., 2017. p. 1948-1951 8054354 (Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017).

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

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AU - Song, Baowei

PY - 2017/9/29

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N2 - High-altitude gliding unmanned underwater vehicles (HAGUUVs) are released in high attitude and works in water after a short glide in the air. According to the High-altitude Gliding UUV airborne emission requirements, the folding mechanism of wings of the HAGUUV is desighed. On the basis of mechanics analysis of the organization, the dynamics modeling of organization's unfolding process is given by using Lagrange equation, and the wings unfolding movement characteristics are discussed through numerical simulation. Analysis results show that the designed folding mechanism can achieve the requirement of High-altitude gliding system performance, and provides theoretical guidance for further drop experiment.

AB - High-altitude gliding unmanned underwater vehicles (HAGUUVs) are released in high attitude and works in water after a short glide in the air. According to the High-altitude Gliding UUV airborne emission requirements, the folding mechanism of wings of the HAGUUV is desighed. On the basis of mechanics analysis of the organization, the dynamics modeling of organization's unfolding process is given by using Lagrange equation, and the wings unfolding movement characteristics are discussed through numerical simulation. Analysis results show that the designed folding mechanism can achieve the requirement of High-altitude gliding system performance, and provides theoretical guidance for further drop experiment.

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KW - Folding wing

KW - High-altitude gliding

KW - Numerical simulation

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Li Y, Song B. Folding mechanism design and analysis of high-altitude gliding UUV wings. In Xu B, editor, Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017. Institute of Electrical and Electronics Engineers Inc. 2017. p. 1948-1951. 8054354. (Proceedings of 2017 IEEE 2nd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2017). doi: 10.1109/IAEAC.2017.8054354

Folding mechanism design and analysis of high-altitude gliding UUV wings

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