Dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing UAV1

Dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing UAV1

The batch launch of small folding-wing UAVs by high altitude balloon at high altitude is a new technology in recent years. The wing deployment process at 20km altitude is analyzed, and mathematical model of the wing delivery is established. Using the multibody dynamics analysis software ADAMS simula...

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Bibliographic Details
Main Authors: Zhang Hangyue, Yang Yanchu
Format: Article
Language:English
Published: EDP Sciences 2018-01-01
Series:MATEC Web of Conferences
Online Access:https://doi.org/10.1051/matecconf/201819805004
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spelling doaj-f086f84807bd4d86996dbea6fcd0e4a72021-02-02T06:05:53ZengEDP SciencesMATEC Web of Conferences2261-236X2018-01-011980500410.1051/matecconf/201819805004matecconf_meae2018_05004Dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing UAV1Zhang HangyueYang YanchuThe batch launch of small folding-wing UAVs by high altitude balloon at high altitude is a new technology in recent years. The wing deployment process at 20km altitude is analyzed, and mathematical model of the wing delivery is established. Using the multibody dynamics analysis software ADAMS simulate the wing deployment process in order to verify the correctness of the model established. Then, the impact of the wing with final velocity on the fuselage is analyzed, and an elastic locking mechanism is designed to reduce the impact. The analysis process provides a certain reference for the task design of balloon-UAVs and the folding mechanism analysis.https://doi.org/10.1051/matecconf/201819805004
collection DOAJ
language English
format Article
sources DOAJ
author Zhang Hangyue
Yang Yanchu
spellingShingle Zhang Hangyue
Yang Yanchu
Dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing UAV1
MATEC Web of Conferences
author_facet Zhang Hangyue
Yang Yanchu
author_sort Zhang Hangyue
title Dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing UAV1
title_short Dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing UAV1
title_full Dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing UAV1
title_fullStr Dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing UAV1
title_full_unstemmed Dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing UAV1
title_sort dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing uav1
publisher EDP Sciences
series MATEC Web of Conferences
issn 2261-236X
publishDate 2018-01-01
description The batch launch of small folding-wing UAVs by high altitude balloon at high altitude is a new technology in recent years. The wing deployment process at 20km altitude is analyzed, and mathematical model of the wing delivery is established. Using the multibody dynamics analysis software ADAMS simulate the wing deployment process in order to verify the correctness of the model established. Then, the impact of the wing with final velocity on the fuselage is analyzed, and an elastic locking mechanism is designed to reduce the impact. The analysis process provides a certain reference for the task design of balloon-UAVs and the folding mechanism analysis.
url https://doi.org/10.1051/matecconf/201819805004
work_keys_str_mv AT zhanghangyue dynamicanalysisofwingdeploymentofhighaltitudeballoonlaunchedsmallsizefoldingwinguav1
AT yangyanchu dynamicanalysisofwingdeploymentofhighaltitudeballoonlaunchedsmallsizefoldingwinguav1
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