Design and Simulation of Ornithopter based on Four-bar Mechanism

In order to study the twin joint structure of bird wings,a flapping wing structure based on four-bar mechanism is designed based on the principle of bionics. The brushless motor driving two stage reducer,provides input for four-bar mechanism. The robot has a function of the periodic flapping motion,...

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Main Authors: Zhao Zhifang, Qi Mingsi, Feng Jingkai, Zhang Wei, Wang Junyuan, Zhang Jiping
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Transmission 2017-01-01
Series:Jixie chuandong
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Online Access:http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2017.11.017
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author Zhao Zhifang
Qi Mingsi
Feng Jingkai
Zhang Wei
Wang Junyuan
Zhang Jiping
author_facet Zhao Zhifang
Qi Mingsi
Feng Jingkai
Zhang Wei
Wang Junyuan
Zhang Jiping
author_sort Zhao Zhifang
collection DOAJ
description In order to study the twin joint structure of bird wings,a flapping wing structure based on four-bar mechanism is designed based on the principle of bionics. The brushless motor driving two stage reducer,provides input for four-bar mechanism. The robot has a function of the periodic flapping motion,the frequency change and size of the attitude angle adjustment. According to the range of bird joint angular motion,the output angle of the robot linkage mechanism is determined so that it can move within the expected range. The model is established by MATLAB/SimMechanics,and the four-bar mechanism of the robot is simulated and integrated into the iSIGHT software to optimize the parameters and obtain the design variable value similar to the expected trajectory. The results show that the ornithopter scheme design based on the design of the four-link mechanism is feasible,and the frequency is controllable. In addition,the optimized simulation curve can well approach the given task trajectory. The design method proposed in this paper has the characteristics of fast and efficient,and the result is intuitively visible,which provides a feasible scheme for parameter setting and optimization of other mechanical structure.
format Article
id doaj-art-0face00f300143ddb9f9f11bb7dfcc6c
institution Kabale University
issn 1004-2539
language zho
publishDate 2017-01-01
publisher Editorial Office of Journal of Mechanical Transmission
record_format Article
series Jixie chuandong
spelling doaj-art-0face00f300143ddb9f9f11bb7dfcc6c2025-01-10T14:20:29ZzhoEditorial Office of Journal of Mechanical TransmissionJixie chuandong1004-25392017-01-0141879129933344Design and Simulation of Ornithopter based on Four-bar MechanismZhao ZhifangQi MingsiFeng JingkaiZhang WeiWang JunyuanZhang JipingIn order to study the twin joint structure of bird wings,a flapping wing structure based on four-bar mechanism is designed based on the principle of bionics. The brushless motor driving two stage reducer,provides input for four-bar mechanism. The robot has a function of the periodic flapping motion,the frequency change and size of the attitude angle adjustment. According to the range of bird joint angular motion,the output angle of the robot linkage mechanism is determined so that it can move within the expected range. The model is established by MATLAB/SimMechanics,and the four-bar mechanism of the robot is simulated and integrated into the iSIGHT software to optimize the parameters and obtain the design variable value similar to the expected trajectory. The results show that the ornithopter scheme design based on the design of the four-link mechanism is feasible,and the frequency is controllable. In addition,the optimized simulation curve can well approach the given task trajectory. The design method proposed in this paper has the characteristics of fast and efficient,and the result is intuitively visible,which provides a feasible scheme for parameter setting and optimization of other mechanical structure.http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2017.11.017Four-bar mechanismOrnithopterBionicMATLAB/SimMechanics iSIGHTParameter optimization
spellingShingle Zhao Zhifang
Qi Mingsi
Feng Jingkai
Zhang Wei
Wang Junyuan
Zhang Jiping
Design and Simulation of Ornithopter based on Four-bar Mechanism
Jixie chuandong
Four-bar mechanism
Ornithopter
Bionic
MATLAB/SimMechanics iSIGHT
Parameter optimization
title Design and Simulation of Ornithopter based on Four-bar Mechanism
title_full Design and Simulation of Ornithopter based on Four-bar Mechanism
title_fullStr Design and Simulation of Ornithopter based on Four-bar Mechanism
title_full_unstemmed Design and Simulation of Ornithopter based on Four-bar Mechanism
title_short Design and Simulation of Ornithopter based on Four-bar Mechanism
title_sort design and simulation of ornithopter based on four bar mechanism
topic Four-bar mechanism
Ornithopter
Bionic
MATLAB/SimMechanics iSIGHT
Parameter optimization
url http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2017.11.017
work_keys_str_mv AT zhaozhifang designandsimulationofornithopterbasedonfourbarmechanism
AT qimingsi designandsimulationofornithopterbasedonfourbarmechanism
AT fengjingkai designandsimulationofornithopterbasedonfourbarmechanism
AT zhangwei designandsimulationofornithopterbasedonfourbarmechanism
AT wangjunyuan designandsimulationofornithopterbasedonfourbarmechanism
AT zhangjiping designandsimulationofornithopterbasedonfourbarmechanism